Chronology - Quarter 3 1964 home
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1964 July 1 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -.
  • Point Arguello transferred to Air Force Nation: USA. Point Arguello (nearly 20,000 acres) transferred from the Navy to the Air Force and annexed to Vandenberg AFB. References: 88.
1964 July 1 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1964 July -
  • Apollo Logistic Support System Office investigates extensions of Apollo hardware. Nation: USA. Spacecraft: Apollo LM Truck. The recent creation of the Apollo Logistic Support System Office in Washington prompted the formal investigation of a variety of extensions of Apollo hardware to achieve greater scientific and exploratory dividends from Apollo hardware. Director of Special Manned Space Flight Studies William B. Taylor suggested to William E. Stoney and others in Houston that Grumman receive a study contract to investigate possible modifications to the lunar excursion module (LEM) to create a LEM truck (concepts which the company had already investigated preliminarily on an in-house basis). The time was appropriate, Taylor said, for more intensive and formal efforts along these lines.
1964 Q3 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Aero High. FAILURE: Failure.
  • Test mission Nation: Australia. Agency: WRE. Apogee: 0 km ( mi). References: 2.
1964 Q3 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Aero High. FAILURE: Failure.
  • Test mission Nation: Australia. Agency: WRE. Apogee: 0 km ( mi). References: 2.
1964 July 1 - 11:16 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. LV Configuration: Voskhod 11A57 T15000-04.
  • Cosmos 34 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: NII-88. Perigee: 201 km (124 mi). Apogee: 342 km (212 mi). Inclination: 64.90 deg. Period: 89.90 min. COSPAR: 1964-034A. USAF Sat Cat: 822. Duration: 8.00 days. Decay Date: 1964-07-09. High resolution photo reconnaissance satellite; returned film capsule References: 2, 6.
1964 July 2 - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-10.
  • Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 July 2 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-58.
  • Ballistic Aeronomy mission Nation: USA. Agency: Sandia. Apogee: 298 km (185 mi). References: 2.
1964 July 2 - 23:59 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 409 / Agena D 2315.
  • OPS 3395 Nation: USA. Payload: Ferret 6 / Agena D 2315. Mass: 1,500 kg (3,300 lb). Class: Sigint. Spacecraft: Ferret. Agency: NRO/USAF. Perigee: 502 km (311 mi). Apogee: 520 km (320 mi). Inclination: 82.10 deg. Period: 94.90 min. COSPAR: 1964-035A. USAF Sat Cat: 824. Decay Date: 1969-08-07. References: 2, 6.
1964 July 5 - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache.
  • Aeronomy mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1964 July 6 -
  • Voskhod crews selected. Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 1. Kamanin select Volynov, Katys, and Yegorov as the prime crew for the Voskhod flight. Komarov, Feoktistov, and Sorokin will be the backup crew. Lazarev will serve as reserve for both crew physician position. The VVS leadership approves the selection. For the first space walk (the flight designated Vykhod at the time), Belyayev, Leonov, Khrunov, and Gorbatko are in training. All want to be first, but Kamanin finds Leonov and Khrunov to have the best analytical minds, to be able to get themselves out of a jam if something goes wrong. He selects Belyayev and Gorbatko to be trained as spacecraft commanders for the missions. References: 376.
1964 July 6 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-62.
  • Ballistic (Sun) Solar mission Nation: USA. Agency: Sandia. Apogee: 288 km (178 mi). References: 2.
1964 July 6 - 18:51 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena D. LV Configuration: Atlas Agena D 352D / Agena D S01A 4807.
  • KH 7-09 Nation: USA. Payload: KH-7 no. 9. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-7. Agency: NRO/USAF. Perigee: 121 km (75 mi). Apogee: 345 km (214 mi). Inclination: 92.90 deg. Period: 89.10 min. COSPAR: 1964-036A. USAF Sat Cat: 825. Decay Date: 1964-07-08. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
  • OPS 4923 Nation: USA. Payload: EHH A3. Mass: 80 kg (176 lb). Class: Sigint. Spacecraft: SSF. Agency: NRO/USAF. Perigee: 156 km (96 mi). Apogee: 505 km (313 mi). Inclination: 92.90 deg. Period: 91.10 min. COSPAR: 1964-036B. USAF Sat Cat: 826. Decay Date: 1965-01-03. Radar monitoring. References: 2, 6, 172, 278.
1964 July 6 - 19:23 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C ESRO S01/1.
  • MPE Ba-7 Aeronomy mission Nation: Europe. Agency: ESRO. Apogee: 198 km (123 mi). References: 2.
1964 July 7 - 19:00 GMT - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1007.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 July 7 - 22:43 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NB3.164.
  • Crab nebula lunar occulation X-ray astronomy mission Nation: USA. Agency: NRL. Apogee: 295 km (183 mi). References: 2.
1964 July 8 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-155.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 July 8 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-232.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 July 8 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-295.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 July 8 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Terrier Tomahawk. LV Configuration: Terrier Tomahawk Sandia 152-63. FAILURE: Failure.
  • Terihawk-12 Aeronomy mission Nation: USA. Agency: Sandia. Apogee: 1.00 km (0.60 mi). References: 2.
1964 July 8 - 19:22 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C ESRO S01/2.
  • MPE Ba-8 Aeronomy mission Nation: Europe. Agency: ESRO. Apogee: 183 km (113 mi). References: 2.
1964 July 8 - 21:02 GMT - Launch Site: Delamar Dry Lake DZ. Launch Complex: -. Launch Pad: 37.3 N x 114.9 W. Launch Vehicle: X-15. LV Configuration: X-15 3-30-50. FAILURE: MH-96 guidance malfunction.
  • X-15A Hor Scan/MH-96 test Nation: USA. Agency: NASA/USAF. Apogee: 51 km (31 mi). Maximum Speed - 5664 kph. Maximum Altitude - 51938 m. First test of IR horizon scanner. References: 2.
1964 July 8 - 21:23 GMT - Launch Site: Green River. Launch Complex: Pad 1. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena A003.
  • USAF A003 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 260 km (160 mi). References: 2.
1964 July 9 - Launch Site: Jiuquan. Launch Complex: LA3. Launch Pad: -. Launch Vehicle: DF-2. Model: DF-2.
  • Test mission Nation: China. Agency: PRC. Apogee: 200 km (120 mi). References: 2.
1964 July 9 - 04:13 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.154UE.
  • Airglow Aeronomy mission Nation: USA. Agency: NASA. Apogee: 167 km (103 mi). References: 2.
1964 July 9 - 08:39 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 141.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 111 km (68 mi). References: 2.
1964 July 9 - 19:00 GMT - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 973.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 July 10 - 21:51 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8K72K.
  • Elektron 3 Nation: USSR. Program: Elektron. Payload: 2D s/n 3. Mass: 350 kg (770 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Elektron-A. Agency: NII-88. Perigee: 408 km (253 mi). Apogee: 6,302 km (3,915 mi). Inclination: 60.90 deg. Period: 159.30 min. COSPAR: 1964-038A. USAF Sat Cat: 829. Studied inner Van Allen belt. Electron 3 and 4 launched by a single carrier rocket. Simultaneous study of the inner and outer radiation belts of the earth, cosmic rays and the upper atmosphere. References: 2, 6.
  • Elektron 4 Nation: USSR. Program: Elektron. Payload: 2D s/n 4. Mass: 444 kg (978 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Elektron-B. Agency: NII-88. Perigee: 447 km (277 mi). Apogee: 66,269 km (41,177 mi). Inclination: 60.80 deg. Period: 1,313.80 min. COSPAR: 1964-038B. USAF Sat Cat: 830. Decay Date: 1983-10-12. Studied outer Van Allen belt. Electron 3 and 4 launched by a single carrier rocket. Simultaneous study of the inner and outer radiation belts of the earth, cosmic rays and the upper atmosphere. References: 2, 6.
1964 July 10 - 23:15 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 404 / Agena D 1177.
  • KH-4A 1008 Nation: USA. Payload: KH-4A s/n 1008 / Agena D 1117. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 173 km (107 mi). Apogee: 346 km (214 mi). Inclination: 84.90 deg. Period: 89.70 min. COSPAR: 1964-037A. USAF Sat Cat: 828. Decay Date: 1964-08-06. KH-4A. Cameras operated satisfactorily, some light leaks. References: 2, 6.
1964 July 11 - Launch Vehicle: Titan. Model: Titan 2.
  • Gemini launch vehicle 2 arrived at Eastern Test Range. Nation: USA. Stage I was erected at complex 19 on July 13, stage II on July 14. Electrical power was applied to the vehicle on July 20 in preparation for Subsystems Functional Verification Tests, which began July 21.
1964 July 11 - Launch Site: Jiuquan. Launch Complex: LA3. Launch Pad: -. Launch Vehicle: DF-2. Model: DF-2.
  • Test mission Nation: China. Agency: PRC. Apogee: 200 km (120 mi). References: 2.
1964 July 11 - 02:02 GMT - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: -. Launch Vehicle: Lambda. Model: Lambda 3. LV Configuration: Lambda 3 L-3-1.
  • Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 857 km (532 mi). References: 2.
1964 July 13 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 861.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 July 13 - 03:04 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 130.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 122 km (75 mi). References: 2.
1964 July 14 -
  • Douglas six-man space research station. Nation: USA. Spacecraft: MORL. A study submitted to NASA by Douglas Aircraft Company concluded that a six-man space research station, capable of orbiting for one year, could be orbiting the Earth within five years. The crew, serving on a staggered schedule, would travel to and from the station on modified Gemini or Apollo spacecraft. The station would provide a small degree of artificial gravity by rotating slowly and would include a centrifuge to simulate reentry forces.
1964 July 14 - 03:00 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 131.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 122 km (75 mi). References: 2.
1964 July 15 - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sirocco. LV Configuration: Sirocco LW-4. FAILURE: Failure.
  • Test mission Nation: USA. Agency: DASA. Apogee: 9.00 km (5.50 mi). References: 2.
1964 July 15 - 00:58 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.49CA.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 191 km (118 mi). References: 2.
1964 July 15 - 02:19 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 133.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 106 km (65 mi). References: 2.
1964 July 15 - 04:09 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.50CA.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 192 km (119 mi). References: 2.
1964 July 15 - 08:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.144UI.
  • Sunrise Ionosphere 1 Ionosphere mission Nation: USA. Agency: NASA. Apogee: 154 km (95 mi). References: 2.
1964 July 15 - 08:05 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.51CA.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 190 km (110 mi). References: 2.
1964 July 15 - 09:06 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.52CA.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 191 km (118 mi). References: 2.
1964 July 15 - 09:20 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.145UI.
  • Sunrise Ionosphere 2 Ionosphere mission Nation: USA. Agency: NASA. Apogee: 161 km (100 mi). References: 2.
1964 July 15 - 10:25 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.146UI.
  • Sunrise Ionosphere 3 Ionosphere mission Nation: USA. Agency: NASA. Apogee: 171 km (106 mi). References: 2.
1964 July 15 - 11:31 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. LV Configuration: Vostok 8A92 R15001-03.
  • Cosmos 35 Nation: USSR. Payload: Zenit-2 11F61 s/n 21. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: NII-88. Perigee: 218 km (135 mi). Apogee: 258 km (160 mi). Inclination: 51.30 deg. Period: 89.20 min. COSPAR: 1964-039A. USAF Sat Cat: 833. Duration: 8.00 days. Decay Date: 1964-07-23. Area survey photo reconnaissance satellite. References: 2, 6,93.
1964 July 15 - 17:30 GMT - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-18.
  • LRL SAP Camera Test / technology mission Nation: USA. Agency: Sandia. Apogee: 270 km (160 mi). References: 2.
1964 July 16 - 02:13 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 134.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 106 km (65 mi). References: 2.
1964 July 16 - 05:30 GMT - Launch Site: Carnarvon. Launch Complex: CARN. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 136.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 114 km (70 mi). References: 2.
1964 July 16 - 16:22 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.127GI.
  • Antenna impedance Ionosphere mission Nation: USA. Agency: NASA. Apogee: 137 km (85 mi). References: 2.
1964 July 16 - 16:54 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-19.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 July 16 - 17:24 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-3. FAILURE: Failure.
  • Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1964 July 17 - 05:15 GMT - Launch Site: Carnarvon. Launch Complex: CARN. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 137.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 120 km (70 mi). References: 2.
1964 July 17 - 08:22 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena D. LV Configuration: Atlas Agena D 216D / Agena D 1802.
  • Vela 3 Nation: USA. Payload: Vela 2A. Mass: 220 kg (480 lb). Class: Surveillance. Type: Nuclear Detection. Spacecraft: Vela. Agency: USAF. Perigee: 102,500 km (63,600 mi). Apogee: 104,101 km (64,685 mi). Inclination: 39.10 deg. Period: 6,024.80 min. COSPAR: 1964-040A. USAF Sat Cat: 836. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
  • Vela 4 Nation: USA. Payload: Vela 2B. Mass: 220 kg (480 lb). Class: Surveillance. Type: Nuclear Detection. Spacecraft: Vela. Agency: USAF. Perigee: 92,103 km (57,230 mi). Apogee: 114,000 km (70,000 mi). Inclination: 40.80 deg. Period: 6,004.30 min. COSPAR: 1964-040B. USAF Sat Cat: 837. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
  • TRS 6 Nation: USA. Payload: ERS 13. Mass: 12 kg (26 lb). Class: Technology. Spacecraft: TRS. Agency: USAF. Perigee: 217 km (134 mi). Apogee: 104,665 km (65,035 mi). Inclination: 36.70 deg. Period: 2,366.20 min. COSPAR: 1964-040C. USAF Sat Cat: 838. Decay Date: 1966-07-01. Decay date suspect Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
1964 July 17 - 08:24 GMT - Launch Site: Cape Canaveral. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache Missile compression.
  • REDLAMP Test / aeronomy mission Nation: USA. Agency: USAF. Apogee: 105 km (65 mi). References: 2.
1964 July 19 - Launch Vehicle: N1, Proton, R-56, UR-700. 1964 July 19 - Launch Site: Shijiedu. Launch Complex: -. Launch Pad: -. Launch Vehicle: T-7. Model: T-7A-S.
  • Life Science (mice) Biological mission Nation: China. Agency: Shanghai. Apogee: 70 km (43 mi). References: 2.
1964 July 10-25 - Launch Vehicle: Titan. Model: Titan 2.
  • Gemini Program Office reported that tests had been conducted on section I of the fuel cells planned for the long-duration Gemini-Titan 5 mission. Nation: USA. Spacecraft: Gemini. Flight: Gemini 5. These tests had resulted in a failure characterized by output decay. A complete investigation was in process to determine the cause of the failure.
1964 July 20 - 10:53 GMT - Launch Site: Wallops Island. Launch Complex: LA3A. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-4. LV Configuration: Scout X-4 S124R.
  • SERT 1 Technology mission Nation: USA. Agency: NASA. Apogee: 4,002 km (2,486 mi). Suborbital 30 minute test of NASA SERT ion engine. The early part of the flight was dedicated to attempts to operate the cesium engine. The cesium engine could not be started because of a high-voltage electrical short circuit. The mercury engine was started about 14 minutes into the flight. This engine was successfully operated for 31 minutes with 53 high-voltage recycle vents which were handled by the fault protection system. Each of the recycle events was only a few seconds duration. Major results from the test were the first demonstration of an ion engine in space, demonstration of effective ion beam neutralization, no EMI effects on other spacecraft systems, and effective recovery from electrical breakdowns. Thrust was measured using three independent measuring systems, and there were no major differences between in-space and ground test performance. References: 2.
1964 July 20 - 17:30 GMT - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-20.
  • LRL SAP Camera Technology mission Nation: USA. Agency: Sandia. Apogee: 287 km (178 mi). References: 2.
1964 July 21 -
  • Orbital laboratory using Apollo-developed components for military applications. Nation: USA. Spacecraft: Apollo X. Commenting on Republican Presidential candidate Barry Goldwater's views on the space program, Warren Burkett, science writer for the Houston Chronicle, observed that a great deal of research being conducted as part of NASA's Apollo program could be of direct value to the military services. Burkett contended that an orbital laboratory using Apollo-developed components could be used for such military applications as patrol and orbital interception. He suggested that, with Apollo, NASA was generating an inventory of 'off-the-shelf' space hardware suitable for military use if needed.
1964 July 21 - Launch Vehicle: N1. 1964 July 21 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1964 July 21 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-31.
  • LASL Sun Solar mission Nation: USA. Agency: Sandia. Apogee: 270 km (160 mi). References: 2.
1964 July 22 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-33.
  • LASL Sun Solar mission Nation: USA. Agency: Sandia. Apogee: 321 km (199 mi). References: 2.
1964 July 22 - 02:50 GMT - Launch Site: Niijima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Lambda. Model: LS-A. LV Configuration: LS-A-1.
  • Test mission Nation: Japan. Agency: STA. Apogee: 150 km (90 mi). References: 2.
1964 July 22 - 08:55 GMT - Launch Site: Niijima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Lambda. Model: LS-A. LV Configuration: LS-A-2.
  • Test mission Nation: Japan. Agency: STA. Apogee: 150 km (90 mi). References: 2.
1964 July 22 - 15:39 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2G. LV Configuration: Thor DSV-2G 250.
  • ASSET 3 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 71 km (44 mi). Suborbital test of small scale spaceplane model to test materials for the X-20 Dynasoar. Aero-thermodynamic structural test vehicle (ASV) for heat shield tests. Launched after four hours of holds. Tested Dynasoar hardware - tungsten nose cap, molbdenum panels with vapor-deposited disilicide, and liquid-cooled double-walled cockpit bathtub panel. Reached 5,500 m/s and recovered near Ascension Island 12 hours after launch. References: 2.
1964 July 23 - 18:43 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.107GE.
  • CR nuclei Cosmic rays mission Nation: USA. Agency: NASA. Apogee: 233 km (144 mi). References: 2.
1964 July 24 -
  • Voskhod flight slips Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 1. Crew training is proceeding normally and the crews will be ready by the scheduled 1 August date. On the other hand the date for launch of the first manned mission has slipped from 15 August well into September. References: 376.
1964 July 25 - 17:35 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.108GE.
  • CR nuclei Cosmic rays mission Nation: USA. Agency: NASA. Apogee: 215 km (133 mi). References: 2.
1964 July 26 - 09:07 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 8L. LV Configuration: Kappa 8L K-8L-4.
  • Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 124 km (77 mi). References: 2.
1964 July 26 - 10:51 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 8L. LV Configuration: Kappa 8L K-8L-5.
  • Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 112 km (69 mi). References: 2.
1964 July 27 -
  • Space simulator plans Nation: USSR. Spacecraft: TMK-1, TMK-E, LK-1, Soyuz A, Soyuz 7K-LOK, LK. A two-day conference is held at IAKM to review requirements for trainers and task simulators over the next 6 to 7 years. The plan includes basic instructional versions of planned spacecraft, trainers for flying around the moon, and a mock-up of the TMK Heavy Interplanetary Spacecraft. These will require a new facility of to 7,000 square metres. Trainers and strands at TsPK will be housed in building D, a hangar-type facility. The TBK-60 thermal/barometric chamber will be housed in a single hangar. To fully specify TsPK trainers and stands for the lunar mission, trainers for space navigation, and military combat spacecraft will not be completed until 1965. References: 376.
1964 July 27 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 617.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 July 28 - 02:08 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-160. LV Configuration: S-160 PT-160-1.
  • Propellant test Nation: Japan. Agency: ISAS. Apogee: 44 km (27 mi). References: 2.
1964 July 28 - 16:50 GMT - Launch Site: Cape Canaveral. Launch Complex: LC12. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 250D (AA9) / Agena B 6009 (AA9).
  • Ranger 7 Nation: USA. Program: Ranger. Mass: 362 kg (798 lb). Class: Planetary. Type: Lunar. Spacecraft: Ranger 6-7-8-9. Agency: NASA/JPL. COSPAR: 1964-041A. USAF Sat Cat: 842. Decay Date: 1964-07-31. First successful Ranger; returned 4,308 photos before lunar impact. The Atlas- Agena B inserted the Agena and Ranger into a 192 km altitude Earth parking orbit. Half an hour after launch a second burn of the Agena engine injected the spacecraft into a lunar intercept trajectory. After separation from the Agena, the solar panels were deployed, attitude control activated, and spacecraft transmissions switched from the omniantenna to the high-gain antenna. The next day the planned mid-course maneuver was successfully initiated at 10:27 GMT. The only anomaly during flight was a brief loss of two-way lock on the spacecraft by the DSIF tracking station at Cape Kennedy following launch.

    Ranger 7 reached the Moon on 31 July. The F-channel began its one minute warm up 18 minutes before impact. The first image was taken at 13:08:45 GMT at an altitude of 2110 km. Transmission of 4,308 photographs of excellent quality occurred over the final 17 minutes of flight. The final image taken before impact had a resolution of 0.5 meters. The spacecraft encountered the lunar surface in direct motion along a hyperbolic trajectory, with an incoming asymptotic direction at an angle of -5.57 degrees from the lunar equator. The orbit plane was inclined 26.84 degrees to the lunar equator. After 68.6 hours of flight, Ranger 7 impacted in an area between Mare Nubium and Oceanus Procellarum (subsequently named Mare Cognitum) at approximately 10.35 S latitude, 339.42 E longitude. Impact occurred at 13:25:48.82 GMT at a velocity of 2.62 km/s. References: 2, 6, 278, 296.

1964 July 28 - 20:06 GMT - Launch Site: White Sands. Launch Complex: LC33. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache.
  • Sphere Aeronomy mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1964 July 28 - 21:14 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 300. LV Configuration: Aerobee 300 NASA 06.10GA.
  • Thermosphere probe Aeronomy mission Nation: USA. Agency: NASA. Apogee: 322 km (200 mi). References: 2.
1964 July 29 - 09:22 GMT - Launch Site: Vandenberg. Launch Complex: 576A3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 248D.
  • NTMP KX-13 Target mission Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1964 July 29 - 09:30 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache.
  • Sphere Aeronomy mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1964 July 29 - 10:07 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-5.
  • Chemical release mission Nation: Japan. Agency: ISAS. Apogee: 300 km (180 mi). References: 2.
1964 July 29 - 19:55 GMT - Launch Site: Hidden Hills DZ. Launch Complex: -. Launch Pad: 36.1 N x 116.0 W. Launch Vehicle: X-15. LV Configuration: X-15 3-31-52.
  • X-15A Heat tran/Local Flow test Nation: USA. Agency: NASA/USAF. Apogee: 23 km (14 mi). Maximum Speed - 5250 kph. Maximum Altitude - 23774 m. First test of various heat-resistant panels attached to fuselage. References: 2.
1964 July 30 - Launch Vehicle: Titan. Model: Titan 2.
  • Gemini missions beyond the 12 originally planned considered. Nation: USA. In response to a request from NASA Headquarters, Gemini Program Office (GPO) provided a study for Gemini missions beyond the 12 originally planned. 'The Advanced Gemini Missions Conceptual Study' described 16 further missions, including a space station experiment, a satellite chaser mission, a lifeboat rescue mission, and both a circumlunar and lunar orbiting mission. On February 28, 1965, GPO reported that a preliminary proposal for Gemini follow-on missions to test the land landing system had not been approved. Spare Gemini launch vehicles 13, 14, and 15 were canceled, and there were no current plans for Gemini missions beyond the approved 12-flight program.
1964 July 30 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-14.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 July 30 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-32.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 July 30 - Launch Site: Vandenberg. Launch Complex: 395-D. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-28.
  • Cobra Skin Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). Demonstration and shakedown operations launch References: 2.
1964 July 30 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-48.
  • Density Aeronomy mission Nation: USA. Agency: Sandia. Apogee: 311 km (193 mi). References: 2.
1964 July 30 - 03:36 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1.
  • Cosmos 36 Nation: USSR. Program: DS. Payload: DS-P1-Yu s/n 1. Mass: 325 kg (716 lb). Class: Military. Type: Target. Spacecraft: DS-P1-Yu. Agency: MO SSSR. Perigee: 253 km (157 mi). Apogee: 488 km (303 mi). Inclination: 49.00 deg. Period: 92.00 min. COSPAR: 1964-042A. USAF Sat Cat: 844. Completed Operations Date: 1965-02-27. Decay Date: 1965-02-28. Development of systems for air defence and the control of outer space. References: 2, 6, 99.
1964 July 31 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1964 August 1 - Launch Vehicle: N1, Proton.
  • Full scale development of Soviet manned lunar flyby and landing projects authorised. Nation: USSR. Program: Lunar L1, Lunar L3. Spacecraft: LK-1, Soyuz 7K-LOK, LK, Luna Ye-8, Soyuz A. Flight: Soyuz A-1, Soyuz A-2, Soyuz A-3, Soyuz A-4. Central Committee of the Communist Party and Council of Soviet Ministers Decree 655-268 'On Work on the Exploration of the Moon and Mastery of Space--piloted LK-1 circumlunar and L3 lunar landing projects and the Ye-6M lunar lander' was issued. Chelomei was to develop the three-stage UR-500K booster and LK-1 spacecraft for the manned lunar flyby. Korolev was to develop the totally different N1 booster and L3 spacecraft complex for the manned lunar landing. First launch of the N1 was to be by the first quarter 1966, with manned lunar landings in 1967 to 1968. Reprioritization led to work being stopped on Korolev's Zvezda 6-man orbiting weapons platform by mid-1965, after a huge mockup had been built.

    Korolev felt that if he had the full support of the Communist Party, the military, and industry he could achieve this goal, and this decree ordered such support. The USSR would be first on the moon. But in truth the draft project behind the decree had not solved all of the technical problems, or provided a solution on how to achieve the required payload on either the booster or spacecraft side. New technology features required for success of the scheme included an advanced guidance system in the N1 third stage equipment bay, the enormous fuel tanks in the N1 first stage, and the Lox/LH2 fuel cells needed for the LOK lunar orbiter. But the real technical problem with the N1-L3 design was the total lack of any weight growth reserve. Even thought the systems had not even been developed yet, engineers were fighting over tens of grams in their weight allocations, let alone the kilograms normally at issue.

    Development of Korolev's Soyuz A-B-V, a competing circumlunar project, was evidently still authorised, although it duplicated Chelomei's LK-1. References: 75, 367, 474.

1964 August 1 - Launch Site: Vik. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 1. LV Configuration: Dragon D-10.
  • FU-125 ionosphere / particles Aeronomy /ionosphere mission Nation: France. Agency: CNES. Apogee: 440 km (270 mi). References: 2.
1964 August 1 - 05:54 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: -. Launch Vehicle: UR-200. Model: UR-200.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 686 km (426 mi). References: 2.
1964 August 3 -
  • Preliminary draft report of the Ad Hoc Astronomy Panel of the Orbiting Research Laboratory (ORL). Nation: USA. Spacecraft: LORL. Willis B. Foster, Director of Manned Space Science in the Office of Space Science and Applications, distributed a preliminary draft report of the Ad Hoc Astronomy Panel of the Orbiting Research Laboratory (ORL). The panel, which met on 26 October 1963 and again on 24 June 1964, was created to sound out the American scientific community on the validity of manned astronomy in space and to define astronomy objectives for the ORL, mission. Additional Details: Preliminary draft report of the Ad Hoc Astronomy Panel of the Orbiting Research Laboratory (ORL)..
1964 August 3 -
  • Voskhod state commission formed. Nation: USSR. Spacecraft: Voskhod. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On formation of the State Commission for Voskhod' was issued. References: 474.
1964 August 5 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-43.
  • LASL Sun Solar mission Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi). References: 2.
1964 August 5 - 02:00 GMT - Launch Site: Baikonur. Launch Complex: LC67/22. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67.
  • POR state trials missile launch Nation: USSR. Agency: RVSN. Apogee: 1,493 km (927 mi). References: 2.
1964 August 5 - 17:15 GMT - Launch Site: Woomera. Launch Complex: LA5B. Launch Pad: LA5B?. Launch Vehicle: Black Knight. Model: Black Knight 301/C2. LV Configuration: Black Knight-301/C2 BK.19.
  • Dazzle re-entry vehicle test Nation: UK. Agency: RAE. Apogee: 602 km (374 mi). References: 2.
1964 August 5 - 23:15 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 413 / Agena D 1605.
  • KH-4A 1009 Nation: USA. Payload: KH-4A s/n 1009 / Agena D 1605. Mass: 1,540 kg (3,390 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 182 km (113 mi). Apogee: 436 km (270 mi). Inclination: 80.00 deg. Period: 90.70 min. COSPAR: 1964-043A. USAF Sat Cat: 846. Decay Date: 1964-09-01. KH-4A. Cameras operated successfully. References: 2, 6.
1964 August 6 - 16:30 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-7.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 August 6 - 23:29 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.55DA.
  • K64-S-1 Air sampling Aeronomy mission Nation: USA. Agency: NASA. Apogee: 125 km (77 mi). References: 2.
1964 August 7 - Launch Site: Vik. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 1. LV Configuration: Dragon D-11.
  • FU-125 ionosphere / particles Aeronomy /ionosphere mission Nation: France. Agency: CNES. Apogee: 420 km (260 mi). References: 2.
1964 August 7 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 998.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 August 7 - 00:16 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.138GA.
  • K64-G-1 Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 130 km (80 mi). References: 2.
1964 August 7 - 01:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.78GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 119 km (73 mi). References: 2.
1964 August 7 - 20:12 GMT - Launch Site: Vandenberg. Launch Complex: 576E. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 110F.
  • Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,400 km (800 mi). References: 2.
1964 August 8 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-42.
  • LASL Sun Solar mission Nation: USA. Agency: Sandia. Apogee: 307 km (190 mi). References: 2.
1964 August 8 - 04:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.104GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 139 km (86 mi). References: 2.
1964 August 9 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1964 August 10 - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 34.0 N x 123.0 W. Launch Vehicle: Iris. Model: Hydra-Iris. LV Configuration: Hydra-Iris GSP-1.
  • LRL GSP-1 Magnetospheric mission Nation: USA. Agency: USN NMC. Apogee: 200 km (120 mi). References: 2.
1964 August 11 - Launch Site: Vandenberg. Launch Complex: 395-C. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-9.
  • Double Talley Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). Demonstration and shakedown operations launch References: 2.
1964 August 11 - 02:00 GMT - Launch Site: Baikonur. Launch Complex: LC67/22. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. FAILURE: Failure.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1964 August 11 - 05:10 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL301.
  • LUX Solar AC1 Solar x-ray and ultraviolet mission Nation: Australia. Agency: WRE/RAE. Apogee: 145 km (90 mi). References: 2.
1964 August 11 - 10:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.82GG.
  • Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 172 km (106 mi). References: 2.
1964 August 12 -
  • Voskhod State Commission Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 1. The readiness of two crews is certified (the prime crew of Volynov, Katys, and Yegorov and backup crew of Komarov, Feoktistov, and Sorokin). Korolev presses for Feoktistov to be included in the prime crew, citing his unequalled technical knowledge of the spacecraft. Kamanin and the VVS doctors oppose this, citing his poor medical condition which makes him uncertifiable for flight. A very heated discussion ensues, with the final decision to continue training all seven cosmonauts, with the first candidates for flight being Volynov, Katys, and Yegorov, with Komarov, Lazarev, and Sorokin being reserve cosmonauts. The question of Feoktistov's flight certification will be taken up by a special panel of physicians. References: 376.
1964 August 12 - 00:43 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.56DA.
  • K64-S-2 Air sampling Aeronomy mission Nation: USA. Agency: NASA. Apogee: 121 km (75 mi). References: 2.
1964 August 12 - 01:49 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.84GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 114 km (70 mi). References: 2.
1964 August 12 - 02:15 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.105GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 126 km (78 mi). References: 2.
1964 August 12 - 18:12 GMT - Launch Site: Hidden Hills DZ. Launch Complex: -. Launch Pad: 36.1 N x 116.0 W. Launch Vehicle: X-15. LV Configuration: X-15 3-32-53.
  • X-15A Heat tran/LF/BLN test Nation: USA. Agency: NASA/USAF. Apogee: 24 km (14 mi). Maximum Speed - 5688 kph. Maximum Altitude - 24750 m. References: 2.
1964 August 13 - Launch Site: Vandenberg. Launch Complex: 395-B. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-7.
  • Gentle Annie Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi). Demonstration and shakedown operations launch References: 2.
1964 August 14 - 09:36 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. LV Configuration: Vostok 8A92 R15001-04.
  • Cosmos 37 Nation: USSR. Payload: Zenit-2 11F61 s/n 22. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: NII-88. Perigee: 208 km (129 mi). Apogee: 240 km (140 mi). Inclination: 64.90 deg. Period: 88.90 min. COSPAR: 1964-044A. USAF Sat Cat: 848. Duration: 8.00 days. Decay Date: 1964-08-22. Area survey photo reconnaissance satellite. Program partially completed. Break in the film fof the SA-10 camera. References: 2, 6,93.
1964 August 14 - 17:54 GMT - Launch Site: Delamar Dry Lake DZ. Launch Complex: -. Launch Pad: 37.3 N x 114.9 W. Launch Vehicle: X-15. LV Configuration: X-15 2-33-56. FAILURE: Nose gear deployed at Mach 4.2.
  • X-15A-2 Stability test Nation: USA. Agency: NASA/USAF. Apogee: 31 km (19 mi). Maximum Speed - 5776 kph. Maximum Altitude - 31486 m. Nose landing gear extended at Mach 4.5. Both tires blew on landing. References: 2.
1964 August 14 - 22:00 GMT - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3 Agena D. LV Configuration: SLV-3 Agena D 7101 / Agena D S01A 4808.
  • KH 7-10 Nation: USA. Payload: KH-7 no. 10. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-7. Agency: NRO/USAF. Perigee: 165 km (102 mi). Apogee: 300 km (180 mi). Inclination: 95.40 deg. Period: 89.10 min. COSPAR: 1964-045A. USAF Sat Cat: 850. Decay Date: 1964-08-23. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
  • OPS 3316 Nation: USA. Payload: P-11 s/n 4202. Mass: 79 kg (174 lb). Class: Sigint. Spacecraft: SSF. Agency: USAF. Perigee: 272 km (169 mi). Apogee: 3,751 km (2,330 mi). Inclination: 95.70 deg. Period: 127.40 min. COSPAR: 1964-045B. USAF Sat Cat: 851. Decay Date: 1979-03-08. References: 2, 6, 172, 278.
1964 August 15 - Launch Vehicle: Proton. Model: Proton 8K82K.
  • Chief Designers review of Voskhod at OKB-1 Nation: USSR. Program: Voskhod. Spacecraft: Voskhod, LK-1. Flight: Voskhod 1. All concerned designers, bureaux, and institutes certify the reliability of the systems of the spacecraft and launch vehicle. The second phase of trials of the soft landing system have been successful. Of 10 drops, 9 landed with vertical velocity under 7.5 m/s, and of those, 6 landed with a speed of only 0.0 to 1.5 m/s. There are still concerns about how the system will function in soft soils or adverse weather conditions. Nevertheless the decision is taken to ship the spacecraft to the cosmodrome for final preparations between 18 and 25 August. It is likely that the manned flight cannot occur until the end of September. Later in the day Kamanin is visited by Sergei Nikitovich Khrushchev and other experts from Chelomei's design bureau. They brief Kamanin on plans for a manned circumnavigation of the moon using their spacecraft launched by their UR-500 booster by the end of 1967. References: 376.
1964 August 16 - Launch Vehicle: Titan. Model: Titan 2.
  • Martin-Baltimore received the propellant tanks for Gemini launch vehicle 6 from Martin-Denver, which had begun fabricating them in April. Nation: USA. Flight: Gemini 6. After being inspected, the tanks were placed in storage where they remained until December 18.
1964 August 16 - 00:53 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.57DA.
  • K64-S-3 Air sampling Aeronomy mission Nation: USA. Agency: NASA. Apogee: 119 km (73 mi). References: 2.
1964 August 16 - 01:13 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.140GA.
  • K64-G-3 Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 135 km (83 mi). References: 2.
1964 August 16 - 03:15 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.85GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 122 km (75 mi). References: 2.
1964 August 16 - 05:53 GMT - Launch Site: Ascension. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.115GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 123 km (76 mi). References: 2.
1964 August 17 -
  • Apollo X spacecraft to be used in Earth orbit for extended duration biomedical and scientific flights. Nation: USA. Spacecraft: Apollo X. MSC's Spacecraft Integration Branch proposed an Apollo 'X' spacecraft to be used in Earth orbit for biomedical and scientific missions of extended duration. The spacecraft would consist of the lunar Apollo spacecraft and its systems, with minimum modifications consisting- of redundancies and spares. The concept provided for a first-phase mission which would consider the Apollo 'X' a two-man Earth-orbiting laboratory for a period of 14 to 45 days. The spacecraft would be boosted into a 370-km orbit by a Saturn IB launch vehicle. Additional Details: Apollo X spacecraft to be used in Earth orbit for extended duration biomedical and scientific flights..
1964 August 17 - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 556.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 August 17 - 00:29 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.58DA.
  • K64-S-4 Air sampling Aeronomy mission Nation: USA. Agency: NASA. Apogee: 124 km (77 mi). References: 2.
1964 August 17 - 00:49 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.141GA.
  • K64-G-4 Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 132 km (82 mi). References: 2.
1964 August 17 - 12:55 GMT - Launch Site: Ascension. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.116GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 122 km (75 mi). References: 2.
1964 August 18 - 01:15 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.106GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 124 km (77 mi). References: 2.
1964 August 18 - 01:25 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.113GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 120 km (70 mi). References: 2.
1964 August 18 - 06:05 GMT - Launch Site: Wallops Island. Launch Complex: LA3. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-4A. LV Configuration: Scout X-4A S129R.
  • Reentry 4A Nation: USA. Agency: NASA. Apogee: 183 km (113 mi). Scout launch tested Apollo-type ablator materials at lunar reentry heating levels. References: 2.
1964 August 18 - 09:15 GMT - Launch Site: Baikonur. Launch Complex: LC41/15. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 65S3. LV Configuration: Kosmos 65S3 02L.
  • Cosmos 38 Nation: USSR. Program: Strela. Mass: 50 kg (110 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1. Agency: MO SSSR. Perigee: 203 km (126 mi). Apogee: 766 km (475 mi). Inclination: 56.10 deg. Period: 94.30 min. COSPAR: 1964-046A. USAF Sat Cat: 853. Decay Date: 1964-11-08. References: 2, 6.
  • Cosmos 39 Nation: USSR. Program: Strela. Mass: 50 kg (110 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1. Agency: MO SSSR. Perigee: 205 km (127 mi). Apogee: 792 km (492 mi). Inclination: 56.10 deg. Period: 94.60 min. COSPAR: 1964-046B. USAF Sat Cat: 854. Decay Date: 1964-11-17. References: 2, 6.
  • Cosmos 40 Nation: USSR. Program: Strela. Mass: 50 kg (110 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1. Agency: MO SSSR. Perigee: 206 km (128 mi). Apogee: 737 km (457 mi). Inclination: 56.10 deg. Period: 94.10 min. COSPAR: 1964-046C. USAF Sat Cat: 855. Decay Date: 1964-11-18. References: 2, 6.
1964 August 19 - 12:15 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Delta D. LV Configuration: Thor Delta D 417/D25.
  • Syncom 3 Nation: USA. Payload: Syncom C. Mass: 39 kg (85 lb). Class: Technology. Type: Comsat. Spacecraft: Syncom. Agency: NASA GSF. Perigee: 35,784 km (22,235 mi). Apogee: 35,792 km (22,240 mi). Inclination: 0.10 deg. Period: 1,436.20 min. COSPAR: 1964-047A. USAF Sat Cat: 858. Completed Operations Date: 1974-12-29. Experimental commsat; carried Star Flash experiment. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit at 64 deg W in 1964; 180 deg E in 1964; 25 deg W in 1965; 165 deg E in 1966-1969. Last known longitude (6 December 1974) 6.08 deg W drifting at 0.188 deg W per day. References: 2, 6.
1964 August 19 - 19:51 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Cajun Dart. LV Configuration: Cajun Dart 01.
  • Test mission Nation: USA. Agency: NASA MSFC. Apogee: 75 km (46 mi). References: 2.
1964 August 20 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-33.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 August 20 - 05:36 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL121.
  • X-ray pinhole / ne Ionosphere / solar x-rays mission Nation: Australia. Agency: WRE/RAE. Apogee: 192 km (119 mi). References: 2.
1964 August 20 - 09:02 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 135.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 119 km (73 mi). References: 2.
1964 August 21 -
  • VPK Meeting on Voskhod Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 1. The Military-Industrial Commission, following statements by the Chief Designers, sets the launch of the prototype Voskhod with mannequins for 5 September followed by the manned flight between 15 and 20 September. References: 376.
1964 August 21 - Launch Site: Vandenberg. Launch Complex: LF08. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1072.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 August 21 - 15:45 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 412 / Agena D 1603.
  • KH-5 9066A Nation: USA. Payload: KH-5 s/n 9066A / Agena D 1603. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-5. Agency: NRO/CIA. Perigee: 351 km (218 mi). Apogee: 363 km (225 mi). Inclination: 114.90 deg. Period: 91.70 min. COSPAR: 1964-048A. USAF Sat Cat: 861. Decay Date: 1965-03-31. KH-5. 15% of stellar film degraded by flare. Image smearing on leading edge of main camera film. Final ARGON mission. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
  • Starflash 1B Nation: USA. Spacecraft: Starflash. Agency: USAF. COSPAR: 1964-048xx. USAF Sat Cat: 861. Decay Date: 1965-03-31. References: 2, 279.
1964 August 22 - 07:12 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78. LV Configuration: Molniya 8K78 R103-36.
  • Cosmos 41 Nation: USSR. Program: Molniya. Payload: Molniya-1. Mass: 1,500 kg (3,300 lb). Class: Communications. Spacecraft: Molniya-1. Agency: NII-88. Perigee: 1,023 km (635 mi). Apogee: 39,169 km (24,338 mi). Inclination: 68.40 deg. Period: 714.50 min. COSPAR: 1964-049D. USAF Sat Cat: 869. Successful launch of first Soviet communications satellite. This is the second Molniya launch attempt. (the first was a launch failure). The failure of the antennae to deploy means the spacecraft can only be tested in a limited manner and cannot be used for the planned relay of television. References: 2, 6, 64, 376.
1964 August 22 - 10:15 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.126GG.
  • Ultraviolet Spectra (Venus) Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 123 km (76 mi). References: 2.
1964 August 22 - 11:02 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1.
  • Cosmos 42 Nation: USSR. Program: Strela. Mass: 100 kg (220 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1. Agency: MO SSSR. Perigee: 228 km (141 mi). Apogee: 1,105 km (686 mi). Inclination: 48.90 deg. Period: 98.10 min. COSPAR: 1964-050A. USAF Sat Cat: 864. Decay Date: 1965-12-19. References: 2, 6.
  • Cosmos 43 Nation: USSR. Program: Strela. Mass: 100 kg (220 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1. Agency: MO SSSR. Perigee: 227 km (141 mi). Apogee: 1,093 km (679 mi). Inclination: 48.90 deg. Period: 98.00 min. COSPAR: 1964-050C. USAF Sat Cat: 867. Decay Date: 1965-12-27. References: 2, 6.
1964 August 25 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 989.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 August 25 - 13:43 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-4. LV Configuration: Scout X-4 S134R.
  • Explorer 20 Nation: USA. Program: Explorer. Payload: IE A (S-48 Ionosphere Explorer). Mass: 44 kg (97 lb). Class: Earth. Type: Ionosphere. Spacecraft: IE. Agency: NASA GSF. Perigee: 857 km (532 mi). Apogee: 999 km (620 mi). Inclination: 79.90 deg. Period: 103.60 min. COSPAR: 1964-051A. USAF Sat Cat: 870. Ionospheric research. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1964 August 26 - 17:01 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.34GI.
  • Ionosphere mission Nation: USA. Agency: NASA. Apogee: 154 km (95 mi). References: 2.
1964 August 26 - 18:42 GMT - Launch Site: Hidden Hills DZ. Launch Complex: -. Launch Pad: 36.1 N x 116.0 W. Launch Vehicle: X-15. LV Configuration: X-15 3-33-54.
  • X-15A HT/LF/BLN test Nation: USA. Agency: NASA/USAF. Apogee: 27 km (16 mi). Maximum Speed - 6216 kph. Maximum Altitude - 27737 m. References: 2.
1964 August 27 - Launch Vehicle: Titan. Model: Titan 2.
  • Hurricane Cleo struck the Cape Kennedy area. Nation: USA. Stage II of Gemini launch vehicle (GLV) 2 was deerected and stored; the erector was lowered to horizontal, and stage I was lashed in its vertical position. Stage II was reerected September 1. Power was applied to the launch vehicle September 2, and Subsystem Functional Verification Tests (SSFVT) began September 3. When forecasts indicated that Hurricane Dora would strike Cape Kennedy, both stages of GLV-2 were deerected on September 8 and secured in the Missile Assembly Building. Hurricane Ethel subsequently threatened the area, and both stages remained in the hanger until September 14, when they were returned to complex 19 and reerected. SSFVT, begun again on September 18, ended successfully October 5.
1964 August 27 - 09:54 GMT - Launch Site: Vandenberg. Launch Complex: OSTF1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 57E.
  • ST/KX-48 Target mission Nation: USA. Agency: USAF SAC. Apogee: 1,600 km (900 mi). References: 2.
1964 August 28 - 07:56 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2 Agena B. LV Configuration: Thor SLV-2 Agena B 399 (TA3) / Agena B 6201. FAILURE: Agena-B cut off too early. Partial Failure.
  • Nimbus 1 Nation: USA. Payload: Nimbus A. Mass: 376 kg (828 lb). Class: Earth. Type: Weather. Spacecraft: Nimbus. Agency: NASA GSF. Perigee: 429 km (266 mi). Apogee: 937 km (582 mi). Inclination: 98.70 deg. Period: 98.40 min. COSPAR: 1964-052A. USAF Sat Cat: 872. Decay Date: 1974-05-16. Returned 27,000 cloud cover images. The spacecraft carried an advanced vidicon camera system for recording and storing remote cloudcover pictures, an automatic picture transmission camera for providing real-time cloud cover pictures, and a high-resolution infrared radiometer to complement the daytime TV coverage and to measure nighttime radiative temperatures of cloud tops and surface terrain. A short second-stage burn resulted in an unplanned eccentric orbit. Otherwise, the spacecraft and its experiments operated successfully until September 22, 1964. The solar paddles became locked in position, resulting in inadequate electrical power to continue operations. References: 2, 6.
1964 August 28 - 16:19 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M. LV Configuration: Vostok 8A92M T15000-05.
  • Cosmos 44 Nation: USSR. Payload: Meteor no. 1. Mass: 4,730 kg (10,420 lb). Class: Earth. Type: Weather. Spacecraft: Meteor. Agency: NII-88. Perigee: 599 km (372 mi). Apogee: 778 km (483 mi). Inclination: 65.10 deg. Period: 98.50 min. COSPAR: 1964-053A. USAF Sat Cat: 876. Investigation of the upper atmosphere and outer space. References: 2, 6.
1964 August 29 - 05:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.122GG.
  • AS / E X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 179 km (111 mi). References: 2.
1964 August 29 - 09:36 GMT - Launch Site: Vandenberg. Launch Complex: LC-A. Launch Pad: -. Launch Vehicle: Scout. Model: Blue Scout Jr SLV-1B(m). LV Configuration: Blue Scout Jr SLV-1B(m) 21-2.
  • Ion Engine Test B Technology mission Nation: USA. Agency: USAF. Apogee: 2,000 km (1,200 mi). The launch was designed to provide about 30 minutes of flight above an altitude of 370 km. At seven minutes into the flight the engine was operated with ion beam extraction. Full beam current of 94 mA was achieved about 10 minutes later. During the course of engine operation, an electric field strength meter was used to infer payload floating potential relative to space. Spacecraft potential was about 1000 V negative during most of the engine operation with the filament neutralizer. The absolute value of payload potential was about ten times higher than anticipated, and it was suspected that there was inadequate neutralization of the ion beam. The contact ion engine operated for 19 minutes until spacecraft reentry into the atmosphere. In addition to withstanding the environmental rigors of space flight, the ion propulsion system demonstrated electromagnetic compatibility with other spacecraft subsystems and the ability to regulate and control a desired thrust level. References: 2.
1964 August 31 -
  • Katys deleted from Voskhod prime crew. Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 1. It is discovered that Katys has a brother and sister living in Paris, a fact he did not disclose during the selection process. They left for Paris in 1910, 16 years before Katys was even born. But together with the fact that his father was executed by the Soviet state, it makes him unsuitable to be a cosmonaut. Yegorov and Feoktistov are making serious efforts to be appointed to the crew. Yegorov did poorly in zero-G training and Feoktistov is physically unqualified. Meanwhile TASS, APN, and other Soviet newspapers are stubbornly pursuing information about the crew for the forthcoming flight. Film biographies and press kits are being made of all of the candidates, so that the information can be released once the final crew - whoever they are - are in orbit. But this violation of secrecy disturbs Kamanin. References: 376.
1964 August 31 - 15:46 GMT - Launch Site: Vandenberg. Launch Complex: 576D. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 36F.
  • Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,400 km (800 mi). References: 2.
1964 September 1 - Launch Site: Baikonur. Launch Complex: LC110L. Launch Pad: -. Launch Vehicle: N1.
  • Construction start of N1 launch complex 110 east Nation: USSR. Program: Lunar L3. References: 96.
1964 September 1 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 668.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 September 1 - Launch Site: Cape Canaveral. Launch Complex: LC20. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3A. LV Configuration: Titan IIIA 3A-2. FAILURE: Transtage pressurization failure caused premature shutdown.
  • Titan 3A Transtage 1 Nation: USA. Payload: Transtage 2. Agency: USAF. COSPAR: F640901A. Decay Date: 1964-09-02. References: 126.
1964 September - Launch Vehicle: Atlas. Model: Atlas D.
  • Atlas SMS 564 deactivated. Nation: USA. Warren-1 AFB SMS 564 deactivated References: 4460.
1964 September 1 - 09:19 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL137.
  • Ozone distribution Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 212 km (131 mi). References: 2.
1964 September 2 - 03:08 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.55UG.
  • Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 156 km (96 mi). References: 2.
1964 September 3 - 17:54 GMT - Launch Site: Hidden Hills DZ. Launch Complex: -. Launch Pad: 36.1 N x 116.0 W. Launch Vehicle: X-15. LV Configuration: X-15 3-34-55.
  • X-15A HT/BLN test Nation: USA. Agency: NASA/USAF. Apogee: 23 km (14 mi). Maximum Speed - 5817 kph. Maximum Altitude - 23957 m. References: 2.
1964 September 4 - Launch Vehicle: Titan. Model: Titan 2.
  • Air Force Space Systems Division (SSD), supported by launch vehicle contractors, recommended that Gemini launch vehicle (GLV) 2 be flown as scheduled. Nation: USA. Manned Spacecraft Center had proposed dropping GLV-2 from the Gemini program because of possible ill effects resulting from the electromagnetic incident of August 17 and from Hurricane Cleo. GLV-3 would then be substituted for the second Gemini mission, and the program would be shortened by one flight. After reviewing the incidents, their effects, corrective action, and retesting, SSD, Martin, Aerospace, and Aerojet-General all felt GLV-2 should fly, and NASA accepted their recommendation.
1964 September 4 - 01:20 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 5C. LV Configuration: Skylark-5C SL87A. FAILURE: Failure.
  • Test mission Nation: Australia. Agency: WRE/RAE. Apogee: 182 km (113 mi). References: 2.
1964 September 5 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-13.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 September 5 - 01:23 GMT - Launch Site: Cape Canaveral. Launch Complex: LC12. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 195D (AA10) / Agena B 6501 (AA10).
  • OGO 1 Nation: USA. Payload: OGO A. Mass: 487 kg (1,073 lb). Class: Earth. Type: Magnetosphere. Spacecraft: OGO. Agency: NASA GSF. Perigee: 21,446 km (13,325 mi). Apogee: 127,394 km (79,158 mi). Inclination: 44.60 deg. Period: 3,809.50 min. COSPAR: 1964-054A. USAF Sat Cat: 879. Decay Date: 1980-08-10. Two experiment booms failed to properly deploy, with one of the booms obscuring a horizon scanner's view of earth. As a result, the spacecraft attitude could not be earth oriented and OGO 1 remained spin stabilized at 5 rpm. Nevertheless, data from all 20 experiments on board was received, although at a 'less than expected capacity' from some of them. Twelve of the experiemnts were particle studies and two were magnetic field studies. In addition, there was one experiment for each of the following types of studies: interplanetary dust, VLF, Lyman-alpha, Gegenschein, atmospheric mass, and radio astronomy. During September 1964, acceptable data were received over 70% of the orbital path. By June 1969, data acquisition was limited to 10% of the orbital path. Spacecraft operation was restricted to Spring and Fall due to power supply limitations. There were 11 such 3-month periods prior to the spacecraft being put into stand-by mode on 25 November 1969. By April 1970 the spacecraft perigee had increased to 46,000 km and the inclination had increased to 58.8 deg. All support was terminated November 1, 1971. References: 2, 6, 278.
1964 September 8 -
  • Crash at Fedosiya Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 1. A Voskhod capsule is finally dropped from 10 km altitude in order to test the parachute hatch ejection mechanism. The hatch fails to deploy, the parachute never opens, and the capsule crashes to earth. Korolev claims the test capsule's electrical scheme is not representative of the production capsule, and promises to ship a production representative capsule, which he guarantees will be reliable, to Fedosiya by 22 September. References: 376.
1964 September 8 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 576.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 September 8 - 03:43 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 2. LV Configuration: Black Brant II AK-2A-59. FAILURE: Failure.
  • Ionosphere mission Nation: Canada. Agency: NRCC. Apogee: 20 km (12 mi). References: 2.
1964 September 9 - Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Voskhod preparations Nation: USSR. Program: Voskhod. Spacecraft: Voskhod, Zenit-4. Flight: Voskhod 1. Kamanin arrives at the cosmodrome, only to find the launch of the manned Voskhod delayed to October. The launch of a Zenit-4 spy satellite, that uses the same launch vehicle as planned for Voskhod, has aborted on the pad after the Block A strap-on failed to ignite. This is the first block A failure in over 100 R-7 launches. That evening Kamanin views a launch of an R-36 heavy ICBM. Marshall Krylov reveals it will have a range of 14,000 km with a CEP of under 1 km with a 40 megaton warhead - one missile is sufficient to wipe out a city like New York. Rudenko believes that the victor in any nuclear war will be the one who pushes the button first. Krylov disagrees, saying that if the Americans would launch an attack on Soviet missile forces, the Soviet Union would launch its missiles on a counter-strike before the American missiles arrive - total and senseless destruction. Rudenko believes that Rudenko is more correct, since in the real-world responses will not conform to theoretical possibilities of instant reaction.

    Later the state commission meets to consider the launch of the first Voskhod. The unpleasantness at the landing trials in the Crimea reveal only the inadequacy of the design of the test capsules, and do not reflect the flight system, says Korolev. He certifies the reliability of the Voskhod for flight. The commission decides to set the launch of the next Zenit-4 reconnaissance satellite for 14 September; that of the Voskhod with mannequins on 18-20 September; the definitive landing system trial at Fedosiya on 23 September; and if that is successful, launch of a manned Voskhod by the end of September. References: 376.

1964 September 9 - 02:13 GMT - Launch Site: Baikonur. Launch Complex: LC67/22. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67.
  • POR state trials missile launch Nation: USSR. Agency: RVSN. Apogee: 1,495 km (928 mi). References: 2.
1964 September 10 - Launch Site: Baikonur. Launch Complex: LC41/3. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1964 September 10 - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1024.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 September 12 - Launch Vehicle: CZ, DF-1, DF-2, DF-3, DF-3 Tsien, DF-4.
  • Chinese missiles redesignated and new development plan adopted. Nation: China. Program: Long March. Tsien had conducted a series of meetings with the Chinese leadership during the year to redefine China's missile development plans. There are clashes between Tsien, who favours an American engineering approach, and his staff, who were trained in Russian and favour the Soviet approach. Finally the missiles were defined by their target objectives, and a new development plan was adopted, with definite goals. The 1059 missile (copy of Russian R-2) was redesignated DF-1. The DF-2 was to be improved to carry an atomic bomb to a range sufficient to hit Japan. The DF-3 ICBM was cancelled, and the new DF-3 project would involve development of a nuclear-tipped missile capable of reaching the Philippines (earlier referred to as the DF-1). The DF-4 was to be capable of hitting Guam, and the DF-5 would be an ICBM capable of reaching the United States. The DF-2, DF-3 and DF-4 would use strap-down accelerometer guidance packages, while the DF-5 was to be equipped with a full-fledged inertial guidance unit. References: 87.
1964 September 13 - 02:57 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-1. Model: A-1.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 100 km (60 mi). References: 2.
1964 September 13 - 09:50 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. LV Configuration: Voskhod 11A57 R15001-01.
  • Cosmos 45 Nation: USSR. Program: Voskhod. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: NII-88. Perigee: 203 km (126 mi). Apogee: 311 km (193 mi). Inclination: 64.90 deg. Period: 89.60 min. COSPAR: 1964-055A. USAF Sat Cat: 880. Duration: 5.00 days. Decay Date: 1964-09-18. Flight: Voskhod 1. High resolution photo reconnaissance satellite; returned film capsule; also carried weather experiments. The Zenit-4 launches a day ahead of schedule. The booster rocket performs perfectly as Korolev and Kamanin watch from the veranda of the IP-1 tracking station. This confirms readiness of the same launch vehicle for the Voskhod launch. References: 2, 6, 376.
1964 September 14 - Launch Vehicle: N1, Proton, Soyuz, UR-700.
  • Voskhod abort system Nation: USSR. Program: Voskhod, Lunar L1, Lunar . Spacecraft: Voskhod, LK-1. Flight: Voskhod 1. Kamanin reviews the Voskhod abort system with Korolev. Up to T+27 seconds, there is no possibility of saving the crew in the event of a booster failure; from T+27 seconds to T+44 seconds, escape would be difficult, but is possible; and from T+44 seconds to T+501 seconds abort should be possible, with the capsule landing on Soviet territory. Afterwards, Korolev speaks with Kamanin secretly and privately. Korolev reveals that he has discussed a greater VVS role in space with Marshal Krylov, but that Krylov is adamantly opposed to the VVS assuming such a mission. Korolev is seeking a resolution from the Communist Party that will authorise him to develop a manned lunar flyby and landing system using his N1 booster. He believes that Chelomei's UR-500 booster will not have sufficient payload to mount a manned flyby - a docking in low earth orbit will be required. But Chelomei has rejected the use of docking, and is even designing his UR-700 to allow a lunar landing without the use of docking.

    Finally Korolev gets to the purpose of the secret meeting. He wants Feoktistov to be aboard Voskhod 1, despite the opinion of Kamanin and the physicians. Kamanin reiterates that the most qualified crew would be Komarov, Volynov, and Lazarev; and if he gives in on Feoktistov, then Komarov, Feoktistov, Lazarev. But Korolev is opposed to Lazarev, and insists that the crew should be Komarov, Feoktistov, and Yegorov. From Kamanin's point of view this is flying a space mission with two invalids aboard. Lazarev is a qualified and fit flight surgeon, a qualified pilot as well as a physician with 15 years of research experience in aviation medicine. Korolev is adamant that the two passengers should be civilian, not military. No agreement is possible. References: 376.

1964 September 14 - 22:53 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 405 / Agena D 1178.
  • KH-4A 1010 Nation: USA. Payload: KH-4A s/n 1010 / Agena D 1178. Mass: 1,330 kg (2,930 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 174 km (108 mi). Apogee: 455 km (282 mi). Inclination: 84.90 deg. Period: 90.90 min. COSPAR: 1964-056A. USAF Sat Cat: 882. Decay Date: 1964-10-06. KH-4A. Small out of focus areas on both cameras at random times throughout the mission. References: 2, 6.
1964 September 15 - Launch Site: Vandenberg. Launch Complex: LF08. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1179.
  • OT (ECP VER) operational test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 September 15 - 06:59 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 2. LV Configuration: Black Brant II AD-2A-58.
  • Ionosphere mission Nation: Canada. Agency: NRCC. Apogee: 166 km (103 mi). References: 2.
1964 September 15 - 09:35 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 KP3.5.
  • Zodiacal light Infrared astronomy mission Nation: USA. Agency: KPNO. Apogee: 200 km (120 mi). References: 2.
1964 September 15 - 15:27 GMT - Launch Site: Vandenberg. Launch Complex: 576A1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 245D.
  • ABRES LORV-3 / Pod 26 Re-entry vehicle test Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1964 September 17 - 05:56 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL120.
  • X-ray pinhole / ne Ionosphere / solar x-rays mission Nation: Australia. Agency: WRE/RAE. Apogee: 192 km (119 mi). References: 2.
1964 September 18 -
  • Apollo Mission A-102 / SA-7 Nation: USA. Program: Apollo. Apollo Mission A-102, using BP-15 for the command and service modules (CSM) and SA-7 for the launch vehicle, confirmed Saturn Block II and CSM compatibility as well as the launch escape vehicle system. References: 16.
1964 September 18 -
  • Voskhod State Commission Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 1. The State Commission meets at Baikonur. Chertok advises that the failure of the parachute hatch to jettison in the trials in Fedosiya was due to a serious defect in the schematics of the electrical layout and will not occur again. Korolev declares he is ready to certify Voskhod ready for the final drop test at Fedosiya but would prefer to delay the launch of the spacecraft with mannequins until after the Fedosiya test. The state commission finally agrees to reschedule the launch from 28-30 September, subject to a successful test at Fedosiya on 24-25 September.

    Aftrwards Tyulin calls Korolev, Mrykin, Kerimov, Rudenko, and Kamanin aside. He tells them the Communist Party and Soviet Ministers have now taken a personal interest in the crew selection for Voskhod. Korolev and Kamanin bitterly debate their competing preferred crews. References: 376.

1964 September 18 - 16:22 GMT - Launch Site: Cape Canaveral. Launch Complex: LC37B. Launch Pad: -. Launch Vehicle: Saturn I. Model: Saturn I. LV Configuration: Saturn I-Blk2 SA-7.
  • Saturn 7 Nation: USA. Program: Apollo. Payload: Apollo CSM Boilerplate 15. Mass: 16,700 kg (36,800 lb). Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo CSM. Agency: NASA MSC. Perigee: 181 km (112 mi). Apogee: 215 km (133 mi). Inclination: 31.70 deg. Period: 88.50 min. COSPAR: 1964-057A. USAF Sat Cat: 883. Decay Date: 1964-09-22. Apollo systems test. Third orbital test. First closed-loop guidance test. References: 2, 6, 26, 27.
1964 September 18 - 17:17 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.115NA.
  • Dayglow Aeronomy mission Nation: USA. Agency: NASA. Apogee: 168 km (104 mi). References: 2.
1964 September 18 - 17:25 GMT - Launch Site: Cape Canaveral. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache.
  • REDLAMP / ne, particles Test / aeronomy / ionosphere mission Nation: USA. Agency: USAF CRL. Apogee: 105 km (65 mi). References: 2.
1964 September 21 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-38.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 September 21 - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1108.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 September 22 - 13:10 GMT - Launch Site: Vandenberg. Launch Complex: 576A3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 247D.
  • NTMP KX-19 Target mission Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1964 September 23 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 906.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 September 23 - 20:06 GMT - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3 Agena D. LV Configuration: SLV-3 Agena D 7102.
  • KH 7-11 Nation: USA. Payload: KH-7 no. 11. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-7. Agency: NRO/USAF. Perigee: 143 km (88 mi). Apogee: 303 km (188 mi). Inclination: 92.90 deg. Period: 88.90 min. COSPAR: 1964-058A. USAF Sat Cat: 884. Decay Date: 1964-09-28. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
1964 September 24 -
  • NASA studying the feasibility of a manned orbiting telescope. Nation: USA. Spacecraft: Orbital Workshop. A background briefing for the press regarding astronomy programs was held in Washington. Nancy Roman, who directed the agency's astronomy activities, disclosed that NASA was studying the feasibility of a manned orbiting telescope. Although the telescope would be designed to operate automatically, man would adjust its focus, collect film packets, and make any necessary repairs. The space agency had already invited members of the scientific community to propose astronomical studies suitable for use in space, and several NASA centers were performing related engineering support studies.
1964 September 24 - Launch Vehicle: N1, R-26, R-56, R-9, Tsiklon, UR-100, UR-200, UR-700.
  • Khrushchev visits Baikonur Nation: USSR. Spacecraft: Voskhod, Berkut, LK-700. Flight: Voskhod 2. This was his last visit, just weeks before his overthrow. The Soviet leadership were shown the UR-100 and observed launches of the competing UR-200 and R-36. Khrushchev agreed with the decision to put the R-36 into production instead of Chelomei’s UR-200. He felt he couldn’t turn down Yangel a third time after approving Korolev’s N1 instead of Yangel’s R-56 and Chelomei’s UR-100 instead of Yangel’s R-26. Khrushchev decided to cancel Korolev’s badly behind schedule R-9A, even though Smirnov and Ustinov insisted they wanted it in their arsenal (in May 1965, after Khrushchev’s overthrow, this decision was reversed and the R-9A went into production).

    Khrushchev also visited a secret space fair, with Korolev, Chelomei, Yangel, and Glushko presenting their rockets and spacecraft. Chelomei presented his UR-700 heavy lift design as an alternative to Korolev’s N1. This presentation was a surprise to Ustinov and Dementiev. Khrushchev ordered Chelomei to prepare a draft proposal for the design. Chelomei hoped that 12 to 18 months later, when the UR-700 draft project would be completed, the fallacy of Korolev’s N1 design would be apparent to all. Korolev’s N1 plans were also reviewed and approved at the meeting.

    Over the two days, Khruschev witnessed five launches of rockets by Korolev, Yangel, and Chelomei, all of them successful. Gagarin and Belyayev explained the Vykhod spacecraft to him, and Leonov donned a spacesuit and demonstrated how he would exit into open space form the inflatable airlock and return thereafter. All went very well.

    This was the last time Khrushchev saw the chief designers of the Soviet rocket industry. Despite his support for them not one of them visited him in his retirement. References: 376.

1964 September 24 - 04:42 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL133.
  • Plasma / Solar X Ionosphere / solar x-rays mission Nation: Australia. Agency: WRE/RAE. Apogee: 180 km (110 mi). References: 2.
1964 September 24 - 05:56 GMT - Launch Site: Baikonur. Launch Complex: LC90/20. Launch Pad: -. Launch Vehicle: UR-200. Model: UR-200.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 686 km (426 mi). Demonstration launch witnessed by Khrushchev. References: 2.
1964 September 24 - 12:00 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. LV Configuration: Vostok 8A92 R15001-05.
  • Cosmos 46 Nation: USSR. Payload: Zenit-2 11F61 s/n 23. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: NII-88. Perigee: 211 km (131 mi). Apogee: 264 km (164 mi). Inclination: 51.30 deg. Period: 89.20 min. COSPAR: 1964-059A. USAF Sat Cat: 885. Duration: 8.00 days. Decay Date: 1964-10-02. Area survey photo reconnaissance satellite. Demonstration launch witnessed by Khrushchev. References: 2, 6,93.
1964 September 24 - 16:04 GMT - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 449.
  • Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1964 September 25 - Launch Site: Baikonur. Launch Complex: LC60/8. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • UBP Kedr operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). Demonstration launch witnessed by Khrushchev. References: 2.
1964 September 25 - 04:03 GMT - Launch Site: Baikonur. Launch Complex: LC67/22. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi). Demonstration launch witnessed by Khrushchev. References: 2.
1964 September 26 - 02:15 GMT - Launch Site: Green River. Launch Complex: Pad 2. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena C001. FAILURE: Failure.
  • USAF C001 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1964 September 26 - 03:50 GMT - Launch Site: Kapustin Yar. Launch Complex: LC84. Launch Pad: -. Launch Vehicle: R-5. Model: R-5 VAO. FAILURE: Failure.
  • VAO Ionosphere mission Nation: USSR. Agency: RVSN. Apogee: 500 km (310 mi). References: 2.
1964 September 26 - 12:04 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.13GP-GT.
  • Attitude control test Nation: USA. Agency: NASA. Apogee: 120 km (70 mi). References: 2.
1964 September 27 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • Climate Test operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1964 September 28 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-57.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1964 September 29 - Launch Vehicle: Titan. Model: Titan 2.
  • Gemini Program Manager Charles W. Mathews presented the Gemini Management Panel with the new flight schedule resulting from the lightning strike and hurricane conditions. Nation: USA. Flight: Gemini 3, Gemini 4. The schedule was as follows: Gemini-Titan (GT) 2, November 17; GT-3, January 30, 1965; and GT-4, April 12. For GT-4 through GT-7, three-month launch intervals were planned; for the remainder of the program, these intervals would be reduced to two and one half months.
1964 September 29 -
  • Voskhod launch preparations Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 1. Kamanin meets Korolev at the MIK assembly building at 09:30. Korolev is preoccupied - his wife is in the Kremlin hospital, scheduled for surgery on 1 October. It is a dangerous diversion when all his powers and concentration need to be devoted to clearing the spacecraft for flight. There has been a problem in installing the second seat in the capsule; it won't clear the hatch by 3 mm. At 10:00 Kamanin reviews preparations of the Baikonur recovery forces for a launch abort. He secretly believes, in view of Voskhod's unreliability and unsafe nature, that all such preparations are mainly psychological and of little realistic effectiveness. At 17:00 the State Commission meets to assess launch readiness. Tyulin reveals that the Tral 1P telemetry system aboard Voskhod has failed. The diagnosis is clear, but it will take 6 to 7 days to get a replacement. The tracking ships in the Pacific and Indian Oceans have been there since August, based on Korolev's originally guaranteed launch date. They will run out of supplies by 5-10 October. Finally it is decided that the boosters and spacecraft for both Voskhod missions will be completed in parallel. The launch of the first spacecraft will be will be delayed to 6 October at 10:00 Moscow time. The manned Voskhod will launch no more than six days after the test with mannequins. The tracking ships will be ordered to stay at sea until 15 October. Korolev leaves for Moscow for two days to be with his wife. The second group of cosmonauts are at the cosmodrome to observe spacecraft and launch preparations; now their visit will have to be extended significantly. References: 376.
1964 September 29 - Launch Site: Baikonur. Launch Complex: LC60/6. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1964 September 29 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 994.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1964 September 29 - 04:31 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL132.
  • Ionosphere / solar x-rays mission Nation: Australia. Agency: WRE/RAE. Apogee: 174 km (108 mi). References: 2.
1964 September 29 - 21:00 GMT - Launch Site: Mud Lake DZ. Launch Complex: -. Launch Pad: 37.9 N x 117.1 W. Launch Vehicle: X-15. LV Configuration: X-15 2-34-57. FAILURE: Nose gear scoop door causes handling difficulties.
  • X-15A-2 Stab.,Star tracker test Nation: USA. Agency: NASA/USAF. Apogee: 29 km (18 mi). Maximum Speed - 5699 kph. Maximum Altitude - 29809 m. References: 2.
1964 September 30 -
  • Formal inspection of Block II Apollo CSM mockup Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. NAA conducted formal inspection and review of Block II CSM mockup. References: 16.

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