Chronology - Quarter 4 1963 home
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1963 October 1 - Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
  • Kosmos scientific satellites authorised. Nation: USSR. Spacecraft: DS-1. All-Russian Council of the National Economy (VSNKh) Decree 'Program for Space Investigations With Small Artificial Satellite, Launched on the Kosmos -- On course of work on small satellites at OKB-586' was issued. References: 474.
1963 October 1 - 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.
1963 October - Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D Mercury s/n 144D.
  • Mercury MA-10 (cancelled) Nation: USA. Program: Mercury. Payload: Mercury SC15B. Spacecraft: Mercury. Location of Spacecraft: Ames Research Center, NASA, Moffett Field, California. Crew: Shepard. Flight: Mercury MA-10. Alan Shepard, and others pushed for a six day Mercury 10 endurance mission. This would give America the manned space endurance record for the first time and also cover the biological objectives of the first two Gemini missions. The Mercury 15B capsule had already been modified for long-duration flight and Shepard had the name 'Freedom 7 II' painted on the side. But the risk and work pending on Gemini persuaded NASA managers not to undertake another mission. References: 59.
1963 October 1 - 10:47 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache AC5.477.
  • Firefly IV BECKY Aeronomy mission Nation: USA. Agency: USAF. Apogee: 182 km (113 mi). References: 2.
1963 October 1 - 17:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.78GS.
  • OSO B spectrometer Solar mission Nation: USA. Agency: NASA. Apogee: 219 km (136 mi). References: 2.
1963 October 1 - 19:39 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-222.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 October 2 - 15:10 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7. LV Configuration: Skylark-7 SL81A.
  • Antenna test / SpE Ionosphere mission Nation: Australia. Agency: WRE/RAE. Apogee: 148 km (91 mi). References: 2.
1963 October 4 - Launch Vehicle: N1.
  • Gagarin identified as head of lunar cosmonauts Nation: USSR. Program: Lunar L1. Class: Manned. Type: Spacecraft. Tereshkova announces in Havana that Gagarin head of lunar cosmonaut team. References: 72.
1963 October 4 -
  • Gemini spacecraft No. 1 arrived at Atlantic Missile Range and was transferred to Hangar AF. Nation: USA. Program: Gemini. Spacecraft: Gemini. After a receiving inspection (October 7) and Voltage Standing Wave Ratio Test (October 8), its instrument pallets were removed for laboratory test and checkout (October 9) while the spacecraft was being checked out, weighed, and balanced. Instrument pallets were reinstalled November 26. Individual and integrated communications, instrumentation, and environmental control systems were then performed. Final industrial area testing of the spacecraft concluded with a confidence level test on February 12, 1964.
1963 October 4 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 695.
  • Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1963 October 4 - 04:18 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-41.
  • Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 October 4 - 05:17 GMT - Launch Site: Vandenberg. Launch Complex: OSTF2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 45F. FAILURE: Failure.
  • Research and development launch Nation: USA. Agency: USAF AFSC. References: 2.
1963 October 5 - Launch Site: Fort Wingate. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 2005.
  • Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Successful missile test. Missed aimpoint by 131 m. References: 2.
1963 October 7 -
  • Nikolayev to wed Tereshkova. Nation: USSR. Flight: Vostok 6. Kamanin meets with Nikolayev to discuss the timing for his enforced wedding to Tereshkova. Nikolayev is evasive, doesn't want to set a date, won't give a direct answer. Kamanin points out the wedding will be the subject of a government decree and a precise date must be set. The possible days are limited due to Tereshkova's heavy travel schedule. Nevertheless Nikolayev refuses to commit to a date in October. References: 376.
1963 October 7 - 20:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.36DI.
  • B field probe Magnetosphere mission Nation: USA. Agency: NASA. Apogee: 165 km (102 mi). References: 2.
1963 October 7 - 20:22 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 1-39-63.
  • X-15A Checkout/Opt Deg. Test/Technology mission Nation: USA. Agency: NASA/USAF. Apogee: 23 km (14 mi). Maximum Speed - 4560 kph. Maximum Altitude - 23710 m. References: 2.
1963 October 7 - 21:31 GMT - Launch Site: Vandenberg. Launch Complex: 576B3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 163D. FAILURE: Failure.
  • ST COOL WATER V test Nation: USA. Agency: USAF SAC. Apogee: 10 km (6 mi). References: 2.
1963 October 8 -
  • Joseph F Shea named manager of Apollo Spacecraft Project Office Nation: USA. Program: Apollo. NASA announced the appointment of Joseph F. Shea as ASPO Manager effective October 22. He had been Deputy Director (Systems) in OMSF. George M. Low, OMSF Deputy Director (Programs), would direct the Systems office as well as his own. Robert O. Piland, Acting Manager of ASPO since April 3, resumed his former duties as Deputy Manager. References: 16.
1963 October 8 - 19:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Boosted Arcas.
  • UJO-1 Ionosphere mission Nation: Sweden. Agency: NASA/RTG. Apogee: 89 km (55 mi). References: 2.
1963 October 9 -
  • Douglas Paracone "flying carpet" escape system from orbital space stations. Nation: USA. Spacecraft: Paracone. A 'flying carpet' escape system from orbital space stations had been proposed by Douglas Aircraft Company. The escape system would be a saucer shape that would expand into a blunt-nosed, cone- shaped vehicle 7.6 m across at its base. The vehicle would act as its own brake as it passed through the atmosphere. Reentry heating problems would be met by using fabrics woven with filaments of nickel-based alloys.
1963 October 9 -
  • Kamanin and Gagarin fly to Cuba to join Tereshkova. Nation: USSR. Flight: Vostok 6. Kamanin and Gagarin fly to Cuba to join Tereshkova. Then over the next 13 days on to Mexico, USA, Canada, England, and East Germany. References: 376.
1963 October 9 - 23:14 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.102NA.
  • Release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 158 km (98 mi). References: 2.
1963 October 10 - Launch Site: Hammaguira. Launch Complex: -. Launch Pad: -. Launch Vehicle: Emma. LV Configuration: Emma 04.
  • Aeronomy mission Nation: France. Agency: CNES. Apogee: 55 km (34 mi). References: 2.
1963 October 10 - 23:13 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.103NA.
  • Release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 158 km (98 mi). References: 2.
1963 October 14 - 05:34 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 2. LV Configuration: Black Brant II BB-2A-20.
  • Ionosphere / aurora mission Nation: Canada. Agency: DRTE. Apogee: 145 km (90 mi). References: 2.
1963 October 15 - Launch Vehicle: Titan. Model: Titan 2.
  • Reconsideration of flying Gemini fixes on Titan II development flights. Nation: USA. Personnel from Air Force Space Systems Division (SSD), Air Force Ballistic Systems Division (BSD), and Titan II contractors met in Los Angeles to reconsider flying Gemini launch vehicle (GLV) fixes on Titan II development flights. BSD, which was responsible for the weapon system development program, had halted the installation of GLV fixes on the Titan II flights because of the limited number of flights remaining to qualify the missile. General Bernard A Schriever, Commander of Air Force Systems Command (of which BSD and SSD were subordinate division), intervened in support of an active program to clean up launch vehicle problem areas. The incorporation of GLV fixes on Titan II flights resumed on November 1 with the flight of Titan II N-25.
By the end of 1963 - Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D Mercury s/n 152D.
  • Mercury MA-11 (cancelled) Nation: USA. Program: Mercury. Payload: Mercury SC12B. Spacecraft: Mercury. Location of Spacecraft: NASA’s Garber Facility, Suitland, Md. Crew: Grissom. Flight: Mercury MA-11. From October 25, 1961 until April 1962 NASA’s Mercury program plan included four one-day flights in 1963. By October 1962 the decision had been quietly taken to limit the long-duration flights to only MA-9 and MA-10. MA-10 was fnally cancelled in turn after the successful MA-9 mission.
1963 October 15 - 09:51 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL171.
  • Grenades / Sodium release / Sphere Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 210 km (130 mi). References: 2.
1963 October 15 - 11:48 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7. LV Configuration: Skylark-7 SL169.
  • Grenade / Chaff Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 139 km (86 mi). References: 2.
1963 October 15 - 15:09 GMT - Launch Site: Woomera. Launch Complex: -. Launch Pad: -. Launch Vehicle: HAT.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 80 km (49 mi). References: 2.
1963 October 15 - 15:09 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7. LV Configuration: Skylark-7 SL170.
  • Grenade / Chaff Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 140 km (80 mi). References: 2.
1963 October 15 - 16:05 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.33GS.
  • Solar XRT Solar x-ray mission Nation: USA. Agency: NASA. Apogee: 197 km (122 mi). References: 2.
1963 October 15 - 19:22 GMT - Launch Site: Woomera. Launch Complex: -. Launch Pad: -. Launch Vehicle: HAT.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 80 km (49 mi). References: 2.
1963 October 15 - 19:22 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL168.
  • Grenades / Sodium release / Sphere Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 180 km (110 mi). References: 2.
1963 October 16 - 16:30 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-221.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 October 17 -
  • NASA Astronaut Training Group 3 selected. Nation: USA. The group was selected to provide crew members for planned Apollo missions (then planned as 4 Saturn I missions in 1965, 2-4 Saturn IB missions in 1966, 6 Saturn V missions from 1967).. Qualifications: Qualified jet pilot with minimum 1,000 flight-hours, bachleor's degree in engineering or physical or biological sciences, under 35 years old, under 183 cm height, excellent health. US citizen.. There were 271 applications, 200 from civilians (including two women) and 71 from military pilots (including two African-Americans). President Kennedy pushed for NASA to appoint a black astronaut, but neither of the applicants met the test pilot requirements. Bobby Kennedy arranged for one of these, USAF Captain Edward Dwight, to be enrolled in the USAF Test Pilot school. He graduated, and then had the necessary qualifications. He was 28 years old, an engineering school graduate, and a B-57 bomber command pilot with 2,000 hours flying time. However NASA did not find him as well qualified as other candidates, and he was not among the 32 chosen for final physical and mental tests.

    From these 32, the final 14 were selected. Of them, four would die (two in a T-38 crash, one in a car crash, and one in the Apollo 204 ground fire) before flying in space. All of the ten remaining would fly in the Apollo program.

1963 October 17 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 672.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1963 October 17 - 02:37 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena D. LV Configuration: Atlas Agena D 197D / Agena D 1801.
  • Vela 2 Nation: USA. Payload: Vela 1B. Mass: 220 kg (480 lb). Class: Surveillance. Type: Nuclear Detection. Spacecraft: Vela. Agency: USAF. Perigee: 101,081 km (62,808 mi). Apogee: 116,582 km (72,440 mi). Inclination: 38.70 deg. Period: 6,486.20 min. COSPAR: 1963-039A. USAF Sat Cat: 674. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
  • TRS 5 Nation: USA. Payload: ERS 12. Mass: 2.00 kg (4.40 lb). Class: Technology. Spacecraft: TRS. Agency: USAF. Perigee: 953 km (592 mi). Apogee: 102,372 km (63,610 mi). Inclination: 35.90 deg. Period: 2,319.40 min. COSPAR: 1963-039B. USAF Sat Cat: 675. Decay Date: 1963-06-30. Decay date suspect Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
  • Vela 1 Nation: USA. Payload: Vela 1A. Mass: 220 kg (480 lb). Class: Surveillance. Type: Nuclear Detection. Spacecraft: Vela. Agency: USAF. Perigee: 101,925 km (63,333 mi). Apogee: 116,528 km (72,407 mi). Inclination: 37.80 deg. Period: 6,519.60 min. COSPAR: 1963-039C. USAF Sat Cat: 692. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
1963 October 17 - 10:52 GMT - Launch Site: Woomera. Launch Complex: LA5B. Launch Pad: LA5B?. Launch Vehicle: Black Knight. Model: Black Knight 201. LV Configuration: Black Knight-201 BK.11.
  • Blue Streak test Nation: Europe. Agency: ELDO/RAE. Apogee: 527 km (327 mi). References: 2.
1963 October 17 - 16:50 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.93II.
  • Ionosphere mission Nation: USA. Agency: NASA. Apogee: 187 km (116 mi). References: 2.
1963 October 18 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-9. Model: Romashka. FAILURE: Failure.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1963 October 18 - 07:09 GMT - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI47.
  • Bio (Cat) Life science mission Nation: France. Agency: FR. Apogee: 155 km (96 mi). References: 2.
1963 October 18 - 09:20 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 2. LV Configuration: Black Brant II CC-2A-39.
  • NO2 release Aeronomy mission Nation: Canada. Agency: CARDE. Apogee: 140 km (80 mi). References: 2.
1963 October 18 - 09:29 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. LV Configuration: Vostok 8A92 G15001-01.
  • Cosmos 20 Nation: USSR. Payload: Zenit-2 11F61 s/n 13. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: NII-88. Perigee: 201 km (124 mi). Apogee: 296 km (183 mi). Inclination: 64.80 deg. Period: 89.40 min. COSPAR: 1963-040A. USAF Sat Cat: 673. Duration: 8.00 days. Decay Date: 1963-10-26. Area survey photo reconnaissance satellite. References: 2, 6,93.
1963 October 22 - Launch Site: Plesetsk. Launch Complex: PU11. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • Groza test Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1963 October 23 - 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.
1963 October 24 -
  • NASA-Industry Apollo Executives Group Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The NASA-Industry Apollo Executives Group, composed of top managers in OMSF and executives of the major Apollo contractors, met for the first time. The group met with George E. Mueller, NASA Associate Administrator for Manned Space Flight, for status briefings and problem discussions. In this manner, NASA sought to make executives personally aware of major problems in the program. References: 16.
1963 October 24 - Launch Site: Baikonur. Launch Complex: LC70. Launch Pad: -. Launch Vehicle: R-9.
  • Silo explosion kills 7 at Baikonur Nation: USSR. On 24 October 1963 an R-9 was being prepared for launch in a silo at LC-70. Unknown to the 11 man launch crew, an oxygen leak in the fuelling system had raised the oxygen partial pressure in the silo from the 21% maximum allowed to 32%. Whie the crew was descending in a lift to the 8th level of the silo, a spark from an electrical panel created a fire in the explosive atmosphere, killing seven and destroying the silo. This happened on the same day as the Nedelin disaster three years earlier, and became the cosmodrome's 'Black Day'. Forever after no launches were attempted from Baikonur on October 24.
1963 October 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 October 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 October 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 October 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 October 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 October 24 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 October 24 - Launch Site: Vandenberg. Launch Complex: LC-A. Launch Pad: -. Launch Vehicle: Dac Roc.
  • Aeronomy mission Nation: USA. Agency: USN. Apogee: 50 km (31 mi). References: 2.
1963 October 24 - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. FAILURE: Second stage failed 353 seconds after launch.
  • DS-A1 s/n 4 Nation: USSR. Program: DS. Payload: DS-A1. Class: Technology. Type: Navigation. Spacecraft: DS-A1. Agency: RVSN. COSPAR: F631024A. Carried military experiments to test communications and navigation equipment needed for command and control of Soviet nuclear forces (later used on the Uragan navigation satellites). Also conducted operational monitoring of cosmic rays, radiation from nuclear tests, and natural and artifically-produced radiation belts. References: 2.
1963 October 24 - 05:30 GMT - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI50. FAILURE: Failure.
  • Bio (Cat) Life science mission Nation: France. Agency: FR. Apogee: 88 km (54 mi). References: 2.
1963 October 25 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5B.
  • VAO Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 500 km (310 mi). References: 2.
1963 October 25 - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena D. LV Configuration: Atlas Agena D 224D / Agena D S01A 4703.
  • Agena D Nation: USA. Spacecraft: KH-7. Agency: USAF. Perigee: 116 km (72 mi). Apogee: 276 km (171 mi). Inclination: 99.00 deg. Period: 88.41 min. COSPAR: 1963-041B. USAF Sat Cat: 678. Decay Date: 1963-10-31. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
  • KH 7-03 Nation: USA. Payload: KH-7 no. 3. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-7. Agency: NRO/USAF. Perigee: 123 km (76 mi). Apogee: 312 km (193 mi). Inclination: 99.00 deg. Period: 88.80 min. COSPAR: 1963-041A. USAF Sat Cat: 677. Decay Date: 1963-10-29. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
1963 October 26 - Launch Vehicle: Titan. Model: Titan 2.
  • Gemini launch vehicle 1 arrived at Atlantic Missile Range and was transferred to complex 19. Nation: USA. Stage I was erected in the complete vehicle erector October 28, stage II in the second stage erector October 29. The two stages were cabled together in the side-by-side configuration required for the Sequence Compatibility Firing scheduled for mid-December. A limited Electronic-Electrical Interference Test was completed November 7, and power was applied to the vehicle November 13.
1963 October 26 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-43.
  • Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 October 26 - 02:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 2. LV Configuration: Black Brant II CC-2A-19.
  • Ionosphere / aurora mission Nation: Canada. Agency: DRTE. Apogee: 145 km (90 mi). References: 2.
1963 October 28 - 03:15 GMT - Launch Site: Cape Canaveral. Launch Complex: LC11. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 136F. FAILURE: Failure.
  • ABRES WAC-1 / Pod 21 Reentry test / plume mission Nation: USA. Agency: USAF AFSC. Apogee: 500 km (310 mi). References: 2.
1963 October 29 -
  • The issue of the Nikolayev/Tereshkova wedding has come to a head. Nation: USSR. The wedding has to be arranged with the VVS General Staff in accordance with the resolution of the Central Committee. Kamanin calls Tereshkova and Nikolayev and orders them to decide the issue - the MUST SET A DATE. He is getting ten phone calls a day about it and can resist no longer. References: 376.
1963 October 29 - 02:53 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 2. LV Configuration: Black Brant II CC-2A-40.
  • NO2 release Aeronomy mission Nation: Canada. Agency: CARDE. Apogee: 140 km (80 mi). References: 2.
1963 October 29 - 20:42 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 1-40-64.
  • X-15A Checkout/Opt Deg. Test/Technology mission Nation: USA. Agency: NASA/USAF. Apogee: 22 km (13 mi). Maximum Speed - 4364 kph. Maximum Altitude - 22600 m. References: 2.
1963 October 29 - 21:19 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 386 / Agena D 1601.
  • KH-5 9059A Nation: USA. Payload: KH-5 s/n 9059A/Agena D 1601. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-5. Agency: NRO/CIA. Perigee: 283 km (175 mi). Apogee: 318 km (197 mi). Inclination: 89.90 deg. Period: 90.60 min. COSPAR: 1963-042A. USAF Sat Cat: 681. Decay Date: 1964-01-21. KH-5; deployed ELINT subsatellite. Fourth film payload retrieved in ARGON program. Film comparable to that of 9058A. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
  • Hitch Hiker 2 Nation: USA. Payload: P-11 s/n A3. Mass: 80 kg (176 lb). Class: Sigint. Spacecraft: SSF. Agency: NRO/USAF. Perigee: 288 km (178 mi). Apogee: 581 km (361 mi). Inclination: 90.00 deg. Period: 93.30 min. COSPAR: 1963-042B. USAF Sat Cat: 682. Decay Date: 1965-05-23. Radar monitoring. References: 2, 6, 172.
1963 October 30 - Launch Vehicle: Saturn I. Model: Saturn IB.
  • Manned Saturn I earth orbital flights canceled Nation: USA. Program: Apollo. Spacecraft: Apollo Lunar Landing. NASA canceled four manned earth orbital flights with the Saturn I launch vehicle. Six of a series of 10 unmanned Saturn I development flights were still scheduled. Development of the Saturn IB for manned flight would be accelerated and "all-up" testing would be started. This action followed Bellcomm's recommendation of a number of changes in the Apollo spacecraft flight test program. The program should be transferred from Saturn I to Saturn IB launch vehicles; the Saturn I program should end with flight SA-10. All Saturn IB flights, beginning with SA-201, should carry operational spacecraft, including equipment for extensive testing of the spacecraft systems in earth orbit.

    Associate Administrator for Manned Space Flight George E. Mueller had recommended the changeover from the Saturn I to the Saturn IB to NASA Administrator James E. Webb on October 26. Webb's concurrence came two days later. References: 16.

1963 October 30 -
  • Only at 14:30 due Tereshkova and Nikolayev finally give in. Nation: USSR. Only at 14:30 due Tereshkova and Nikolayev finally give in. The wedding is set for three days later. 300 will attend the wedding, from Khrushchev on down. References: 376.
1963 October 30 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 1. LV Configuration: Dragon D-05.
  • Test mission Nation: France. Agency: CNES. Apogee: 470 km (290 mi). References: 2.
1963 October 30 - 14:26 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL134.
  • Test mission Nation: Australia. Agency: WRE/RAE. Apogee: 186 km (115 mi). References: 2.
1963 October 31 - Launch Vehicle: Saturn V.
  • First production F-1 engine delivered Nation: USA. Program: Apollo. The first production F-1 engine for the Apollo Saturn V was flown from Rocketdyne's Canoga Park, Calif., facility, where it was manufactured, to MSFC aboard Aero Spacelines' "Pregnant Guppy." References: 16.
1963 October 31 -
  • The highest leadership of the Soviet Union is busy making the Nikolayev/Tereshkova wedding arrangements. Nation: USSR. The highest leadership of the Soviet Union is busy making the Nikolayev/Tereshkova wedding arrangements. Tereshkova disappears for four hours during the day and doesn't show up for important meetings. References: 376.
1963 October 31 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 664.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1963 October -
  • Project Luster Nation: USA. Program: Apollo. NASA tentatively approved Project Luster, a program designed to capture lunar dust deflected from the moon by meteorites and spun into orbit around the earth. An Aerobee 150 sounding rocket containing scientific equipment built by Electro-Optical Systems, Inc., was scheduled for launch in late 1964. References: 16.
1963 October 31 - 16:50 GMT - Launch Site: Wallops Island. Launch Complex: LA1. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.94II.
  • Ionosphere mission Nation: USA. Agency: NASA. Apogee: 187 km (116 mi). References: 2.
1963 October 31 - 18:00 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AC6.341.
  • D-region composition Ionosphere mission Nation: USA. Agency: USAF. Apogee: 112 km (69 mi). References: 2.
1963 October 31 - 21:17 GMT - Launch Site: Wallops Island. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.111GT.
  • Vibration test Nation: USA. Agency: NASA. Apogee: 134 km (83 mi). References: 2.
1963 November 1 - Launch Site: White Sands. Launch Complex: LC38. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • Test mission Nation: USA. Agency: USA. Apogee: 200 km (120 mi). References: 2.
1963 November 1 - 08:56 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Sputnik 11A59. LV Configuration: Sputnik 11A59 E15003-02A.
  • Polet 1; Polyot 1 Nation: USSR. Payload: I-2B s/n 1. Mass: 1,400 kg (3,000 lb). Class: Military. Type: ASAT. Spacecraft: Polyot. Agency: NII-88. Perigee: 331 km (205 mi). Apogee: 1,420 km (880 mi). Inclination: 58.90 deg. Period: 102.40 min. COSPAR: 1963-043A. USAF Sat Cat: 683. Decay Date: 1982-10-16. ASAT interceptor control and propulsion test. Launched by Korolev R-7 because Chelomei's own UR-200 was not yet available. Purpose - elaboration of system providing for the extensive manoeuvring of space apparatuses. Flight was considered a great success. Micro-engine fired 350 times and main stabilizing engine fired 300 times. Orbit given is final orbit after manoeuvres. References: 2, 6, 272.
1963 November 1 - 20:15 GMT - Launch Site: Cape Canaveral. Launch Complex: LC15. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-25.
  • Research and development / Pod T test / plume study mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Titan II development flight N-25 was launched from the Atlantic Missile Range. It carried the oxidizer surge chamber and fuel accumulator kit intended to reduce the amplitude of longitudinal vibration which had characterized earlier flights. NASA regarded 0.25g as the maximum level tolerable in manned space flight; this flight achieved a level of 0.22g, the first to fall within acceptable limits. Although the kit had been tested on only one flight, Gemini Project Office had sufficient confidence in it to decide, on November 6, to procure several more such kits for subsequent installation in Gemini launch vehicles. Two later Titan II development flights (N-29 on December 12, 1963, and N-31 on January 15, 1964) and the flight of Gemini-Titan 1 confirmed the validity of this decision. The required kits for the remaining Gemini launch vehicles were then procured. References: 2.
1963 November 2 -
  • Kamanin's phone is ringing off the hook. Nation: USSR. Kamanin's phone is ringing off the hook. Thousands want to attend the wedding - and it turns out there will be only space for 200. Kamanin is taking all the blame for this. References: 376.
1963 November 2 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 613.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1963 November 3 -
  • Nikolayev/Tereshkova wedding Nation: USSR. The wedding, attended by the top leadership of the Soviet Union, goes well. Afterwards the newlyweds continue the party with a friends-only group of 60 at Nikolayev's apartment. References: 376.
1963 November 4 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -.
  • First launch in the ABRES program Nation: USA. First launch in the Advanced Ballistic Reentry System (ABRES) program at Vandenberg AFB. Vehicle used for this mission was an Atlas D. References: 88.
1963 November 4 - 09:34 GMT - Launch Site: Vandenberg. Launch Complex: 576A1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 232D.
  • ABRES REX-III re-entry vehicle test flight Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1963 November 4 - 10:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache Sphere.
  • Aeronomy mission Nation: USA. Agency: USAF. Apogee: 215 km (133 mi). References: 2.
1963 November 4 - 15:10 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 KP3.3.
  • Dayglow Aeronomy mission Nation: USA. Agency: KPNO. Apogee: 200 km (120 mi). References: 2.
1963 November 5 -
  • Khrushchev gives Nikolayev and Tereshkova a new apartment Nation: USSR. Khrushchev has given Nikolayev and Tereshkova a new apartment in Moscow. It is in a building normally reserved exclusively for the highest Communist Part members - Kutuzovskiy Prospect number 30132, Apartment 1013L. The apartment has 7 rooms and can be divided into two sections if they wish to live apart. References: 376.
1963 November 5 - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: -. Launch Vehicle: UR-200. Model: UR-200. LV Configuration: UR-200 No. 01. FAILURE: Failure.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). First UR-200 test flight. (LKI) References: 2.
1963 November 7 -
  • Apollo Pad Abort Mission 1 Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Apollo Pad Abort Mission I (PA-1), the first off-the-pad abort test of the launch escape system (LES), was conducted at WSMR. PA-1 used CM boilerplate 6 and an LES for this test.

    All sequencing was normal. The tower-jettison motor sent the escape tower into a proper ballistic trajectory. The drogue parachute deployed as programmed, followed by the pilot parachute and main parachutes. The test lasted 165.1 seconds. The postflight investigation disclosed only one significant problem: exhaust impingement that resulted in soot deposits on the CM. References: 16.

1963 November 7 - Launch Site: Vandenberg. Launch Complex: LC-A. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3. LV Configuration: Black Brant III AA-3-8?.
  • Test mission Nation: USA. Agency: USN. Apogee: 116 km (72 mi). References: 2.
1963 November 7 - 16:00 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Apollo LES. LV Configuration: Apollo LES PA-1.
  • Test mission Nation: USA. Agency: NASA. Apogee: 2.00 km (1.20 mi). References: 2.
1963 November 7 - 18:11 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 3-23-39.
  • X-15A Sharp Upper Vert. test Nation: USA. Agency: NASA/USAF. Apogee: 25 km (15 mi). Maximum Speed - 4706 kph. Maximum Altitude - 25080 m. First flight with sharp-edged vertical stabilizer. References: 2.
1963 November 8 -
  • Go-ahead to RCA to develop the Apollo LEM radar Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Grumman issued a go-ahead to RCA to develop the LEM radar. Negotiations on the $23.461 million cost- plus-fixed-fee contract were completed on December 10. Areas yet to be negotiated between the two companies were LEM communications, inflight test, ground support, and parts of the stabilization and control systems. References: 16.
1963 November 8 - Launch Vehicle: Saturn I. Model: Saturn IB.
  • Uprated H-1 engine for the first stage of the Saturn IB Nation: USA. Program: Apollo. MSFC directed Rocketdyne to develop an uprated H-1 engine to be used in the first stage of the Saturn IB. In August, Rocketdyne had proposed that the H-1 be uprated from 85,275 to 90,718 kilograms (188,000 to 200,000 pounds) of thrust. The uprated engine promised a 907-kilogram (2,000 pound) increase in the Saturn IB's orbital payload, yet required no major systems changes and only minor structural modifications. References: 16.
1963 November 9 - Launch Site: Vandenberg. Launch Complex: 395-C. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-27.
  • Research and development test Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1963 November 9 - 20:27 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2 Agena D. LV Configuration: Thor SLV-2 Agena D 400 / Agena D 1171. FAILURE: Failure.
  • KH-4 9060 Nation: USA. Payload: KH-4 s/n 9060. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. COSPAR: F631109A. Decay Date: 1963-11-09. KH-4. Mission failed. References: 126.
  • SRV 632 Nation: USA. Spacecraft: KH-4. Agency: USAF. COSPAR: F631109B. References: 279.
1963 November 11 - 06:23 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78. LV Configuration: Molniya 8K78 G103-18. FAILURE: During unpowered coast in parking orbit the escape stage Block L lost stable attitude. Engine ignition occurred in an incorrect direction.
  • Cosmos 21 Nation: USSR. Program: Mars. Payload: 3MV-1A s/n 1. Mass: 890 kg (1,960 lb). Class: Planetary. Type: Venus. Spacecraft: Venera 3MV-1A. Agency: NII-88. Perigee: 192 km (119 mi). Apogee: 231 km (143 mi). Inclination: 64.80 deg. Period: 88.70 min. COSPAR: 1963-044A. USAF Sat Cat: 687. Decay Date: 1963-11-14. The stage with payload remained in Earth orbit as Cosmos-51 and burnt up on re-entry. References: 2, 6, 64, 65.
1963 November 11 - 18:48 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-42.
  • Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 November 12 - Launch Vehicle: Saturn V.
  • Contract for the construction of Saturn V LC-39A Nation: USA. Program: Apollo. NASA awarded a $19.2 million contract to Blount Brothers Corporation and M. M. Sundt Construction Company for the construction of Pad A, part of the Saturn V Launch Complex 39 at LOC. References: 16.
1963 November 12 - 18:58 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.76UA.
  • JHU Airglow 6 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 223 km (138 mi). References: 2.
1963 November 13 - Launch Vehicle: N1.
  • N1 launch site facility construction approved. Nation: USSR. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On approval of the schedule of work for the N1 launch complexes' was issued. References: 474.
1963 November 13 - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 446.
  • Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1963 November 13 - 22:35 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 158D. FAILURE: Failure.
  • ST COOL WATER VI test Nation: USA. Agency: USAF SAC. Apogee: 100 km (60 mi). References: 2.
1963 November 13 - 23:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AD3.324.
  • Dayglow Aeronomy mission Nation: USA. Agency: USAF. Apogee: 262 km (162 mi). References: 2.
1963 November 14 -
  • The resolution is issued on final selection of the second cosmonaut group. Nation: USSR. References: 376.
1963 November 14 -
  • Cancellation of X-20 program proposed. Nation: USA. Spacecraft: Dynasoar, MOL. The Director of Defense for Research and Engineering recommended to the Secretary of Defense cancellation of the X-20 program and initiation of a space station program. Harold Brown believed that Blue Gemini could accommodate significantly greater payload for such missions. He recommended that DynaSoar be cancelled and replaced by a Gemini-serviced space station.
1963 November 14 - Launch Site: Vandenberg. Launch Complex: 395-A1. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I SM-68.
  • Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,000 km (600 mi). References: 2.
1963 November 14 - Launch Site: Kwajalein. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • K-24 Titan Intercept Nation: USA. Agency: USA. Apogee: 200 km (120 mi). References: 2.
1963 November 14 - 19:19 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 1-41-65.
  • X-15A CO/Opt Deg/Systems Test/Technology mission Nation: USA. Agency: NASA/USAF. Apogee: 27 km (16 mi). Maximum Speed - 5287 kph. Maximum Altitude - 27680 m. References: 2.
By the end of 1963 - Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D Mercury s/n 167D.
  • Mercury MA-12 (cancelled) Nation: USA. Program: Mercury. Payload: Mercury SC17. Spacecraft: Mercury. Location of Spacecraft: US Air Force Museum, Wright-Patterson Air Force Base, Dayton, OH. Crew: Schirra. Flight: Mercury MA-12. From October 25, 1961 until April 1962 NASA’s Mercury program plan included four one-day flights in 1963. By October 1962 the decision had been quietly taken to limit the long-duration flights to only MA-9 and MA-10. MA-10 was fnally cancelled in turn after the successful MA-9 mission.
1963 November 16 - Launch Vehicle: Titan. Model: Titan 2.
  • Flight Crew Support Division reported an agreement with Flight Operations Division on a flight profile and rendezvous evaluation experiment for the Gemini-Titan 4 mission. Nation: USA. Flight: Gemini 4. Objective of the experiment was to stimulate normal Agena/Gemini rendezvous and to repeat part of the maneuver using loss of signal/manual technique. Basically, the mission would use circular phasing and catch-up orbit as proposed by the Flight Crew Support Division. Exact fuel requirements and ground tracking requirement were under study by Flight Operations Division.
1963 November 16 -
  • Kuznetsov is named the new chief of the cosmonaut training centre in replacement of Odintsev. Nation: USSR. References: 376.
1963 November 16 - 10:34 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. LV Configuration: Voskhod 11A57 G15000-06.
  • Cosmos 22 Nation: USSR. Payload: Zenit-4 no. 1. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: NII-88. Perigee: 193 km (119 mi). Apogee: 376 km (233 mi). Inclination: 64.90 deg. Period: 90.20 min. COSPAR: 1963-045A. USAF Sat Cat: 689. Duration: 6.00 days. Decay Date: 1963-11-22. High resolution photo reconnaissance satellite; returned film capsule References: 2, 6.
1963 November 16 - 16:55 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-233.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 November 17 - 18:15 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.85NA.
  • Airglow Aeronomy mission Nation: USA. Agency: NASA. Apogee: 370 km (220 mi). References: 2.
1963 November 18 - Launch Site: Vandenberg. Launch Complex: LC-A. Launch Pad: -. Launch Vehicle: Honest John. Model: HJ Nike Nike. LV Configuration: HJ Nike Nike HAD-1.
  • LRL HAD-1 test Nation: USA. Agency: AEC/LRL. Apogee: 163 km (101 mi). References: 2.
1963 November 19 -
  • Plans for the next Vostok flights Nation: USSR. Spacecraft: Vostok. Flight: Vostok 7, Vostok 8, Vostok 9, Vostok 10. Plans for the next Vostok flights are discussed with the training group formed in September. Two group flights of 8 to 10 days each seem the most likely possibility. References: 376.
1963 November 20 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-44.
  • Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 November 21 -
  • Vostok 5/6 cosmonauts' Far East tour Nation: USSR. Spacecraft: Vostok. Flight: Vostok 5, Vostok 6. The cosmonauts are to depart on a Far East tour on 27 November, but scheduling is difficult because Sukarno calls to change the dates for Indonesia nearly daily. Kamanin develops four variant scenarios. The cosmonauts are to visit Sri Lanka, Burma, and Indonesia. References: 376.
1963 November 21 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9a Sandia 152-7.
  • Ballistic test Nation: USA. Agency: Sandia. Apogee: 292 km (181 mi). References: 2.
1963 November 21 - 12:55 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.128IA.
  • ISRO 10.01 (Na) Aeronomy mission Nation: USA. Agency: NASA. Apogee: 208 km (129 mi). References: 2.
1963 November 22 -
  • President Kennedy killed; Lyndon B. Johnson becomes President Nation: USA. President Kennedy shot and killed by sniper in Dallas, Tex. Lyndon B. Johnson becomes President same day
1963 November 22 - 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.
1963 November 22 - 21:00 GMT - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9a Sandia 152-9.
  • HRT test Nation: USA. Agency: Sandia. Apogee: 292 km (181 mi). References: 2.
1963 November 23 -
  • VVS Opposes Further Vostok Flights Nation: USSR. Spacecraft: Vostok. Flight: Vostok 7, Vostok 8, Vostok 9, Vostok 10. News reaches Moscow that Kennedy has been assassinated. Kamanin talks with Rudenko, who is not interested in Kamanin's plans for a wider VVS role in space. Rudenko believes Korolev's promises that Soyuz will start test flights in 1964 and that no further Vostok flights are necessary. Kamanin pleads that without such flights the American Gemini program will fly unopposed and give the Americans a decisive lead in the space race. The Soviet Union could launch a modified Vostok - a three place spacecraft - to upstage Gemini but the decision has to made now. Rudenko is unmoved. References: 376.
1963 November 23 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • State trials flight Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1963 November 24 -
  • North American final report on extended missions for the Apollo spacecraft. Nation: USA. Spacecraft: Apollo X. North American issued the final report of its study for MSC on extended missions for the Apollo spacecraft. In stressing the supreme importance of man's role in the exploration of space-and the uncertainties surrounding the effects of prolonged exposure to the zero-gravity environment of space-the company suggested that an Earth-orbital laboratory would be an ideal vehicle for such long-term experimental evaluation, with missions exceeding a year's duration. Additional Details: North American final report on extended missions for the Apollo spacecraft..
1963 November 25 -
  • Vostok / Soyuz Space Plans Nation: USSR. Spacecraft: Vostok. Kamanin meets with Korolev at OKB-1. Korolev is opposed to the VVS getting out of manned space flight. The Air Force already has a good laboratory infrastructure to support such space flights. More to the point Korolev feels more at home working with pilots and is sick and tired of dealing with the artillery officers that run the rocket forces. He's been stuck with them for twenty years and its a constant stress. A resolution was issued for development of the Soyuz on 1 December. However Korolev needs 80 million roubles to build and fly four Soyuz spacecraft in 1964, but has only been allocated 30 million. References: 376.
1963 November 26 - 18:16 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.10UA.
  • UM Composition 3 / Den Aeronomy mission Nation: USA. Agency: NASA. Apogee: 172 km (106 mi). References: 2.
1963 November 26 - 18:44 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.131UA.
  • Sphere / Structure Aeronomy mission Nation: USA. Agency: NASA. Apogee: 151 km (93 mi). References: 2.
1963 November 27 - Launch Vehicle: Saturn V.
  • First long-duration test firing of Apollo J-2 engine Nation: USA. Program: Apollo. At its Santa Susana facility, Rocketdyne conducted the first long-duration (508 seconds) test firing of a J-2 engine. In May 1962 the J-2's required firing time was increased from 250 to 500 seconds. References: 16.
1963 November 27 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 842.
  • Demonstration and shakedown operations launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1963 November 27 - 02:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta C. LV Configuration: Thor Delta C 387/D21.
  • Explorer 18 Nation: USA. Program: Explorer. Payload: IMP A. Mass: 62 kg (136 lb). Class: Earth. Type: Magnetosphere. Spacecraft: IMP. Agency: NASA GSF. Perigee: 192 km (119 mi). Apogee: 197,616 km (122,792 mi). Inclination: 33.30 deg. Period: 5,666.20 min. COSPAR: 1963-046A. USAF Sat Cat: 693. Decay Date: 1965-11-30. Radiation data; Interplanetary Monitoring Program. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1963 November 27 - 17:50 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NE3.153.
  • Solar extreme ultraviolet mission Nation: USA. Agency: NRL. Apogee: 216 km (134 mi). References: 2.
1963 November 27 - 19:03 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36A. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Centaur. LV Configuration: Atlas Centaur AC-2 / Centaur D 126D.
  • Atlas Centaur 2 Nation: USA. Payload: Centaur 2B. Mass: 4,620 kg (10,180 lb). Class: Planetary. Type: Lunar. Spacecraft: Surveyor. Agency: NASA LeR. Perigee: 469 km (291 mi). Apogee: 1,478 km (918 mi). Inclination: 30.40 deg. Period: 104.60 min. COSPAR: 1963-047A. USAF Sat Cat: 694. Launch vehicle test. Launch vehicle put dummy payload into geosynchronous transfer orbit. First successful Centaur (liquid hydrogen-fueled) flight. References: 2, 6, 278.
1963 November 27 - 20:17 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 3-24-41.
  • X-15A Checkout mission Nation: USA. Agency: NASA/USAF. Apogee: 27 km (16 mi). Maximum Speed - 5326 kph. Maximum Altitude - 27371 m. References: 2.
1963 November 27 - 21:15 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2 Agena D. LV Configuration: Thor SLV-2 Agena D 406 / Agena D 1172.
  • KH-4 9061 Nation: USA. Payload: KH-4 s/n 9061 / Agena D 1172. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: NRO/CIA. Perigee: 182 km (113 mi). Apogee: 368 km (228 mi). Inclination: 69.60 deg. Period: 90.00 min. COSPAR: 1963-048A. USAF Sat Cat: 695. Decay Date: 1963-12-15. KH-4. Mission failed. Return capsule separated from satellite but remained in orbit. References: 2, 6.
1963 November 28 -
  • John F Kennedy Space Center (KSC) named Nation: USA. Program: Apollo. In honor of the late President John F. Kennedy, who was assassinated six days earlier, President Lyndon B. Johnson announced that LOC and Station No. 1 of the Atlantic Missile Range would be designated the John F. Kennedy Space Center (KSC), ". . . to honor his memory, and the future of the works he started . . . ," Johnson said. On the following day, he signed an executive order making this change official. With the concurrence of Florida Governor Farris Bryant, he also changed the name of Cape Canaveral to Cape Kennedy. References: 16.
1963 November 28 -
  • Bykovsky achieved lunar flight duration Nation: USSR. Flight: Vostok 5, Vostok 6. According to a review of Bykovsky's flight log, Bykovsky could have successfully completed a circumlunar flight. Tereshkova would have tired on such a flight - she ate poorly and slept too much. References: 376.
1963 November 28 - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. LV Configuration: Vostok 8A92 G15001-02. FAILURE: Failure of block E upper stage. Spacecraft liquidated by APO destruct system.
  • Zenit-2 11F61 s/n 14 Nation: USSR. Payload: Zenit-2 11F61 s/n 14. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: RVSN. COSPAR: F631128A. Decay Date: 1963-11-28. Area survey photo reconnaissance satellite. References: 93.
1963 November 29 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 642.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1963 November 30 -
  • MOL orbiting laboratory program suggested. Nation: USA. Spacecraft: Dynasoar, MOL. Largely because of NASA objections to the space station proposal, Dr. Brown suggested to the Secretary of Defense an orbiting laboratory program, employing Gemini capsule and a 1,500 cubic foot test module.
1963 November -
  • Apollo LEM tethered flight vehicle considered Nation: USA. Program: Apollo. Spacecraft: Apollo LM. MSC directed Grumman to halt work on LEM test article 9, pending determination of its status as a tethered flight vehicle. As a result, the proposed flight demonstration of the tether coupler, using an S-64A Skycrane helicopter, was canceled. References: 16.
1963 December 1 - Launch Site: Shijiedu. Launch Complex: -. Launch Pad: -. Launch Vehicle: T-7. Model: T-7A.
  • Test mission Nation: China. Agency: Shanghai. Apogee: 115 km (71 mi). References: 2.
1963 December 2 - 04:15 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL135.
  • Test mission Nation: Australia. Agency: WRE/RAE. Apogee: 168 km (104 mi). References: 2.
1963 December 3 - Launch Vehicle: Titan. Model: Titan 2.
  • The Gemini Program Planning Board issued a memorandum of understanding of the correction of the Titan II deficiencies for the Gemini program. Nation: USA. This agreement formalized NASA specifications and Air Force plans to clean up problems related to longitudinal oscillations (POGO), combustion instability, and engine improvement. The program to alleviate the POGO effect included ground proof tests of all subsystems modified to control oscillations. Flight tests of the solutions would be flown on Titan II missiles before application to the Gemini launch vehicle. For the combustion stability program, dynamic stability would be demonstrated through the use of artificially produced disturbances, with the engines being flight tested on unmanned vehicles as final proof of man-rating. Engine improvement was a program to correct all design deficiencies that had cropped up during the Titan II development flights.
1963 December 3 -
  • Soyuz circumlunar spacecraft approved. Nation: USSR. Spacecraft: Soyuz A, Soyuz B, Soyuz V, Soyuz 7K-OK. Decree 'On approval of work on the Soyuz 7K-9K-11K circumlunar complex' was issued. This elaborated on the Soyuz design made under the prior decree of 16 April 1962. Initial design work was authorised on the Soyuz 7K earth orbit basic version - capable of automatic rendezvous and docking with other spacecraft; and the 9K and 11K tanker / refuelable rocket blocks to put the 7K in high altitude or circumlunar orbits. References: 474.
1963 December 3 - 04:59 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL104. FAILURE: Failure.
  • CW / SpE / La / RF / XR Ionosphere / solar x-rays mission Nation: Australia. Agency: WRE/RAE. Apogee: 106 km (65 mi). References: 2.
1963 December 3 - 08:00 GMT - Launch Site: Baikonur. Launch Complex: LC67/21. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. LV Configuration: R-36 8K67 G22500-04L.
  • Kura state trials missile launch Nation: USSR. Agency: RVSN. Apogee: 903 km (561 mi). References: 2.
1963 December 4 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-9. Model: Romashka. FAILURE: Failure.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1963 December 5 - Launch Site: Cuxhaven. Launch Complex: -. Launch Pad: -. Launch Vehicle: Seliger. Model: Seliger Rocket.
  • First Cuxhaven military launches Nation: Germany. The first military launches were made from Cuxhaven since the Backfire V-2 launches of 1945. Seliger, under contract to Waffen und Luftruestung AG (Weapons and Air Development Inc) of Hamburg launched a test rocket. The altitude was restricted to 30 km by a new regulation of the Lower Saxony Economy and Trade Ministry.
1963 December 5 - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150.
  • HR solar spectrum Solar ultraviolet mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1963 December 5 - Launch Site: Cuxhaven. Launch Complex: -. Launch Pad: -. Launch Vehicle: Seliger. Model: Seliger 1.
  • Test mission Nation: Germany. Agency: DRG. Apogee: 30 km (18 mi). References: 2.
1963 December 5 - 19:04 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 1-42-67.
  • X-15A Opt Deg/Sys/Mach 6 Technology/test Nation: USA. Agency: NASA/USAF. Apogee: 30 km (18 mi). Maximum Speed - 6465 kph. Maximum Altitude - 30785 m. Camera test in combination with U-2 flight. References: 2.
1963 December 5 - 21:51 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Ablestar. LV Configuration: Thor Ablestar-2 385 AB015.
  • Transit 5BN-2 Nation: USA. Program: Transit. Mass: 75 kg (165 lb). Class: Navigation. Spacecraft: Transit. Agency: USN. Perigee: 1,061 km (659 mi). Apogee: 1,110 km (680 mi). Inclination: 90.10 deg. Period: 107.00 min. COSPAR: 1963-049B. USAF Sat Cat: 704. Transit operational prototype powered by a SNAP-9A nuclear power source. First operational navigation satellite. It was used regularly by both surface and submarine units of the Navy until November 1964. From this point in time the US Navy had continuous use of satellite navigation. References: 2, 6.
  • Transit 5E-3 Nation: USA. Program: Transit. Mass: 53 kg (116 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Transit. Agency: USN. Perigee: 1,060 km (650 mi). Apogee: 1,108 km (688 mi). Inclination: 90.10 deg. Period: 106.90 min. COSPAR: 1963-049C. USAF Sat Cat: 705. Radiation monitoring. References: 2, 6.
1963 December 7 - 1963 December 7 - 13:11 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.55GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 103 km (64 mi). References: 2.
1963 December 7 - 13:43 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.21UA.
  • UM Pitot 3 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 141 km (87 mi). References: 2.
1963 December 8 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-9. Model: Romashka. FAILURE: Failure.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1963 December 9 - 05:24 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee 200. LV Configuration: Astrobee 200 AC15.610. FAILURE: Failure.
  • Ionization detector Aeronomy / aurora mission Nation: USA. Agency: USAF. Apogee: 242 km (150 mi). References: 2.
1963 December 10 -
  • Cancellation of the X-20 DynaSoar project and start of the MOL project Nation: USA. Spacecraft: Dynasoar, MOL. Secretary of Defense Robert S. McNamara announced cancellation of the X-20 Dyna Soar project at a news briefing at the Pentagon. McNamara stated that fiscal resources thereby saved would be channeled into broader research on the problems and potential value of manned military operations in space, chiefly the Manned Orbiting Laboratory (MOL) project. These decisions on the X-20 and MOL had been discussed and coordinated with NASA, and, although the Air Force received responsibility for the MOL project, NASA would continue to provide technical support. By the end of 1963 $410 million had been spent on Dynasoar, with another $373 million needed through the first flight. It was decided to complete re-entry testing of the Asset subscale unmanned vehicle, at a cost of $ 41 million.
1963 December 10 -
  • MOL development approved Nation: USSR.
1963 December 10 - Launch Site: Vandenberg. Launch Complex: LC-A. Launch Pad: -. Launch Vehicle: Dac Roc.
  • Aeronomy mission Nation: USA. Agency: USN. Apogee: 50 km (31 mi). References: 2.
1963 December 10 - 03:11 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-48.
  • Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 December 11 - Launch Vehicle: Saturn I, Saturn V.
  • Douglas contracted for 10 additional Apollo S-IVB stages Nation: USA. Program: Apollo. NASA Headquarters approved a $48,064,658 supplement to the Douglas Aircraft Company, Inc., contract for 10 additional S-IVB stages, four for the Saturn IB and six for the Saturn V missions. References: 16.
1963 December 11 - Launch Site: White Sands. Launch Complex: LC38. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • Nike X R&D, last WS test Nation: USA. Agency: USA. Apogee: 200 km (120 mi). References: 2.
1963 December 11 - 05:00 GMT - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: -. Launch Vehicle: Lambda. Model: Lambda 2. LV Configuration: Lambda 2 L-2-2.
  • Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 410 km (250 mi). References: 2.
1963 December 12 - Launch Site: Baikonur. Launch Complex: LC41/3. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • Military training launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1963 December 12 - 01:00 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-46. FAILURE: Failure.
  • Test mission Nation: USA. Agency: USN. Apogee: 1.00 km (0.60 mi). References: 2.
1963 December 12 - 08:50 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 8L. LV Configuration: Kappa 8L K-8L-2.
  • Aeronomy / Fields mission Nation: Japan. Agency: ISAS. Apogee: 103 km (64 mi). References: 2.
1963 December 12 - 16:50 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AD3.513.
  • Extreme ultraviolet Mon / XR / RPA Solar extreme ultraviolet mission Nation: USA. Agency: USAF. Apogee: 325 km (201 mi). References: 2.
1963 December 12 - 19:06 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 122.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi). References: 2.
1963 December 12 - 20:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC15. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-29.
  • Research and development / Pod T test / plume study mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1963 December 13 -
  • NASA canceled five Ranger flights Nation: USA. Program: Ranger. Spacecraft: Ranger 6-7-8-9. NASA canceled five Ranger flights (numbers 10 through 14) designed to take high-resolution photographs of the lunar surface before impact. (Five Rangers had thus far been launched.) OSS Associate Administrator Homer E. Newell stated that NASA would depend on the remaining four Rangers, the Lunar Orbiters, and the Surveyors for information about the lunar surface. Cancellation of the flights promised to save $90 million. References: 16.
1963 December 13 - Launch Vehicle: Titan. Model: Titan 2.
  • Martin-Baltimore received the propellant tanks for Gemini launch vehicle (GLV) 3 from Martin-Denver, which had begun fabricating them in June. Nation: USA. Flight: Gemini 3. Splicing the oxidizer and fuel tanks for each stage was completed April 17, 1964. Flight engines arrived from Aerojet-General on May 10, and installation was completed June 6. Final horizontal tests of the assembled launch vehicle began June 1 and were concluded on June 17 with an Air Force inspection of GLV-3 before the vehicle was erected in the vertical test facility.
1963 December 13 - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 854.
  • Demonstration and shakedown operations launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1963 December 13 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 708.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1963 December 13 - Launch Site: Baikonur. Launch Complex: LC67/21. 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.
1963 December 13 - 14:15 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1.
  • Cosmos 23 Nation: USSR. Payload: DS-U / Omega-1. Mass: 347 kg (765 lb). Class: Technology. Spacecraft: Omega. Agency: MO SSSR. Perigee: 232 km (144 mi). Apogee: 560 km (340 mi). Inclination: 48.90 deg. Period: 92.40 min. COSPAR: 1963-050A. USAF Sat Cat: 707. Decay Date: 1964-03-27. Tested VNIIEM electric gyrodyne satellite orientation technology. References: 2, 6.
1963 December 16 -
  • Safety for Apollo of breathing 100 percent oxygen at 5 psi for 30 days proven Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. MSC and the U.S. Air Force Aerospace Medical Division completed a joint manned environmental experiment at Brooks Air Force Base, Tex. After spending a week in a sea-level atmospheric environment, the test subjects breathed 100 percent oxygen at 3.5 newtons per square centimeter (5 psi) at a simulated altitude of 8,230 meters (27,000 feet) for 30 days. They then reentered the test capsule for observation in a sea-level environment for the next five days. This experiment demonstrated that men could live in a 100 percent oxygen environment under these conditions with no apparent ill effects. References: 16.
1963 December 16 -
  • Yerkina wedding Nation: USSR. Program: Soyuz, Lunar L1. Spacecraft: Soyuz A. Flight: Soyuz A-1, Soyuz A-2, Soyuz A-3, Soyuz A-4. The cosmonaut weds at the TsPK cosmonaut centre, and 80 guests attend. Of the female cosmonauts, only Ponomaryova is not yet married. However the next female flight will be made no earlier than 1965-1966. Tereshkova looks tired after her tour to Southeast Asia - and she's supposed to go to Ghana on 10 January! Korolev claims that the Soyuz schedule, as laid out in the resolution of 4 December 1963, is still realistic. He will have the first Soyuz flight in August 1964 and the second and third in September 1964. Ivanovskiy doesn't believe it will be possible to make any flights until 1965. Korolev and Tsybin disccuss Shcherbakov's design for a rocket-propelled high-altitude glider. This concept was supported by the VVS, but Dementiev was against it and it was killed in the bureaucracy. References: 376.
1963 December 17 - Launch Site: Vandenberg. Launch Complex: 395-D. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-28.
  • Research and development / Pod T? test / plume study mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1963 December 17 - 17:17 GMT - Launch Site: Vandenberg. Launch Complex: 4300C. Launch Pad: 4300C. Launch Vehicle: Scout. Model: Blue Scout Jr SLV-1C. LV Configuration: Blue Scout Jr SLV-1C 302.
  • ERCS 279L Communications mission Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). References: 2.
1963 December 18 - 09:52 GMT - Launch Site: Vandenberg. Launch Complex: 576A1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 233D.
  • ABRES LORV-8 re-entry vehicle test flight Nation: