1963 July 1 - -
Vostok 5/6 international press conference Nation: USSR. Spacecraft: Vostok. Flight: Vostok 6, Vostok 5. Big international press conference with the cosmonauts, beginning at 13:00. The session goes 1 hour and 45 minutes and all answers given by the cosmonauts are acceptable. After this conference they disappear from public view for seven days of medical examinations and monitoring.
References: 376.
1963 July 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 July 1 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9a Sandia 152-3. -
Nitehawk-9 test Nation: USA. Agency: Sandia. Apogee: 250 km (150 mi). References: 2.
1963 July 1 - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 431. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1963 July 1-2 - -
Apollo CM boilerplate 6 shipped Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. North American shipped Apollo CM boilerplate 6 and its ground support equipment to WSMR. References: 16.
1963 July 10 - Launch Vehicle: Saturn V. -
Pregnant Guppy FAA certification Nation: USA. Program: Apollo. Aero Spacelines' "Pregnant Guppy," a modified Boeing Stratocruiser, won airworthiness certification by the Federal Aviation Agency. The aircraft would be used to transport major Apollo spacecraft and launch vehicle components. References: 16.
1963 July 2 - -
Yazdovskiy presses complaints about Tereshkova's performance Nation: USSR. Flight: Vostok 6. Doctor Yazdovskiy is insisting that Tereshkova is not being truthful about her flight experience. She handed out rations to on-lookers at the landing site in order to cover up the fact she did not eat enough during the flight. Kamanin considers the accusation a stupidity and indicative of the constant war going on between the flight surgeons and the cosmonauts. Tereshkova powerfully denies the accusation and defends herself well.
References: 376.
1963 July 2 - 14:18 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.14GI. -
Topside sounder Ionosphere mission Nation: USA. Agency: NASA. Apogee: 934 km (580 mi). References: 2.
1963 July 2 - 16:00 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-118. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 July 2 - 16:30 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-167. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 July 3 - -
STL go-ahead to develop a parallel descent engine for the Apollo LEM Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Space Technology Laboratories received Grumman's go-ahead to develop the parallel descent engine for the LEM. At the same time, Grumman ordered Bell Aerosystems Company to proceed with the LEM ascent engine. The contracts were estimated at $18,742,820 and $11,205,415, respectively.
References: 16.
1963 July 3 - -
Cosmonaut controversies Nation: USSR. Flight: Vostok 6, Vostok 5. A fight ensues over the release of the motion picture film of the flight. The Kremlin leadership still does not want to show the 'secret' launch cadres, rocket and spacecraft configurations, etc. There is also conflict with the planned dismissal of cosmonauts Nelyubov, Anikeyev, and Filatyev, with the flown cosmonauts using their connections with the political hierarchy to try and overturn the decisions of their military commanders. Finally, Tereshkova started a campaign to get a posthumous Hero of the Soviet Union medal for cosmonaut parachute trainer Nikitin. This particularly irritated the military command since as far as they were concerned Nikitin died due to his own error and killed another parachutist in the process. In no way was this deserving of a medal, but the award would convey significant financial benefits to his family and Tereshkova fought on. This was indicative of the quick turnaround celebrity brought to the cosmonauts - from obedient junior officers, anxious not to lose a chance for a spaceflight, to aggressive campaigners, willing to take on even members of the General Staff for what they thought was right.
References: 376.
1963 July 3 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Berenice. LV Configuration: Berenice 006. -
Re-entry Vehicle test Nation: France. Agency: ONERA. Apogee: 270 km (160 mi). References: 2.
1963 July 3 - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-26. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 July 3 - 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 July 3 - Launch Site: Kwajalein. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3. -
K-23 Atlas Intercept Nation: USA. Agency: USA. Apogee: 200 km (120 mi). References: 2.
1963 July 3 - 09:00 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AB3.247. -
Structure Test / ionosphere mission Nation: USA. Agency: USAF. Apogee: 199 km (123 mi). References: 2.
1963 July 3 - 21:13 GMT - Launch Site: Vandenberg. Launch Complex: 576C. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 69E. -
Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,600 km (900 mi). References: 2.
1963 July 5 - 21:00 GMT - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 518. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1963 July 6 - 00:36 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5. -
Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 400 km (240 mi). References: 2.
1963 July 7 - -
Kamanin presses for specialised cosmonaut training Nation: USSR. Flight: Vostok 6, Vostok 5. In a two hour meeting with Rudenko, Kamanin attempts to convince him of the need for specialised cosmonaut training (qualifying as spacecraft commander, pilot, navigator, engineer, etc.) for future multi-crew spacecraft. Kamanin points out that in five to seven years they will be routinely flying 2 or 3 place spacecraft and need to start differentiating training now in order to be ready in time. However Rudenko remains unconvinced. Meanwhile Bykovskiy and Tereshkova are at the cosmonaut training centre, completing their flight reports. Kamanin faces difficulties in booking a hotel for the entire cosmonaut group in the Crimea in August --- he can't find any place with fifty vacancies, and concludes he'll have to split the group up. Pressure is coming from the Foreign Ministry for Tereshkova to make an early trip to Brazil, but she is already booked for two or three tours of friendly socialist countries beginning on 30 August and any additional trips can only be made after those are completed.
References: 376.
1963 July 8 - Launch Site: Baikonur. Launch Complex: LC41/15. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Combat training launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1963 July 9 - Launch Site: Baikonur. Launch Complex: LC41/15. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Combat training launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1963 July 9 - 20:12 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 1-37-59. -
X-15A Opt Deg/TravP/RAS Technology/test Nation: USA. Agency: NASA/USAF. Apogee: 69 km (42 mi). Maximum Speed - 5842 kph. Maximum Altitude - 69010 m. References: 2.
1963 July 10 - -
Prototype engine for the Apollo SM reaction control system Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The Marquardt Corporation began testing the prototype engine for the SM reaction control system. Preliminary data showed a specific impulse slightly less than 300 seconds. References: 16.
1963 July 10 - -
Odintsev pressing criticism of Tereshkova Nation: USSR. Flight: Vostok 6. Odintsev is still trying to formally criticise Tereshkova for her flight performance. He charges that she was drunk when she reported to the launch pad and while in orbit was insubordinate, disregarding direct orders from the Centre. Kamanin knows this to be absolutely not true. Both cosmonauts and workers at the cosmonaut training centre report that is impossible to work with Odintsev any more - they want him out.
References: 376.
1963 July 10 - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. LV Configuration: Vostok 8A92 E15000-04. FAILURE: Shutdown of Block B strap-on engine stage 1.9 seconds after liftoff. Pad damaged. -
Zenit-2 11F61 s/n 12 Nation: USSR. Payload: Zenit-2 11F61 s/n 12. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: RVSN. COSPAR: F630710A. Decay Date: 1963-07-10. Area survey photo reconnaissance satellite. References: 93.
1963 July 10 - 02:46 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.59UI. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 204 km (126 mi). References: 2.
1963 July 10 - 17:02 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AC3.511. -
Extreme ultraviolet Mon / RPA Solar ultraviolet mission Nation: USA. Agency: USAF. Apogee: 225 km (139 mi). References: 2.
1963 July 11 - 23:00 GMT - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 650. -
Demonstration and shakedown operations launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1963 July 12 - Launch Vehicle: Titan. Model: Titan 2. -
Effects on pilot performance of longitudinal oscillations (POGO) of the Gemini launch vehicle. Nation: USA. Gemini Project Office (GPO) completed a test program on the centrifuge at Ames Research Center to evaluate the effects on pilot performance of longitudinal oscillations (POGO) of the Gemini launch vehicle. When subjected to oscillatory g-loads ranging from 0 to ± 3g superimposed on a steady-state load of 3.5g, pilot perception and performance decreased markedly above ± 0.25g. Primary effects were impaired pilot vision, reduced eye scan rate, masked sensory perception and kinesthetic cues, and degraded speech. GPO reconfirmed the need to reduce POGO to a maximum of 0.25g.
1963 July 12 - -
Korolev wants review of Tereshkova's flight performance Nation: USSR. Flight: Vostok 6, Vostok 5. Kamanin discusses future cosmonaut book plans with writer Riabchikov. He is interrupted by a call from Korolev. Korolev wants Tereshkova and Bykovskiy in his office the following morning at 10 am sharp and he wants a full explanation for Tereshkova's poor self- samochuviniy on orbits 32 and 42, about her pvote, her poor appetite during the flight, and her failure to complete some assigned tasks. He blames Kamanin for providing her with inadequate training prior to the flight -- which Kamanin finds a joke since he had never received any support in the past from Korolev for his requests for more and better training of the cosmonauts in high-G and zero-G situations. Korolev had also never listened to any of Kamanin's complaints about the need to improve the living conditions for the cosmonaut on the Vostok spacecraft.
References: 376.
1963 July 12 - Launch Site: Kwajalein. Launch Complex: -. 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 July 12 - 20:45 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena D. LV Configuration: Atlas Agena D 201D / Agena D S01A 4702. -
KH 7-01 (Gambit) Nation: USA. Payload: KH-7 no. 1. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-7. Agency: NRO/USAF. Perigee: 173 km (107 mi). Apogee: 212 km (131 mi). Inclination: 95.30 deg. Period: 88.30 min. COSPAR: 1963-028A. USAF Sat Cat: 618. Decay Date: 1963-07-17. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
1963 July 13 - -
Bykovskiy and Tereshkova take their first road trip Nation: USSR. Flight: Vostok 6, Vostok 5. Bykovskiy and Tereshkova take their first road trip, to Yaroslavl. It is clear that Tereshkova is the star and Bykovskiy is in her shadow. Bykovskiy calls Kamanin - he asks that his wife and Tereshkova's brother be allowed to accompany them on their first foreign trip. Kamanin rejects the request.
References: 376.
1963 July 14 - 21:03 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.88CI. -
Eclipse cal Ionosphere mission Nation: USA. Agency: NASA. Apogee: 172 km (106 mi). References: 2.
1963 July 15 - -
271 applications for the astronaut program Nation: USA. Program: Apollo. MSC had received 271 applications for the astronaut program. Seventy-one were military pilots (one from the Army, 34 from the Navy, 26 from the Air Force, and 10 from the Marines). Of the 200 civilians applying, three were women. References: 16.
1963 July 15 - Launch Vehicle: Kosmos 2, Kosmos 3, R-16. -
R-12U, R-14U, and R-16U silo-based missiles accepted into service. Nation: USSR. Decree 'On adoption into armaments of the R-12U, R-14U, and R-16U shaft versions' was issued. References: 474.
1963 July 15-16 - Launch Vehicle: Little Joe II. -
Little Joe II qualification test vehicle shipped Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The Little Joe II qualification test vehicle was shipped from the General Dynamics Convair plant to WSMR, where the test launch was scheduled for August. References: 16.
1963 July 16 - -
Five men began a 30-day engineering test of life support systems for a manned space station in The Boeing Company space chamber. Nation: USA. At Seattle, five men began a 30-day engineering test of life support systems for a manned space station in The Boeing Company space chamber. The system, designed and built for NASA's Office of Advanced Research and Technology, was the nation's first to include all life-support equipment for a multimanned, long-duration space mission (including environmental control, waste disposal, and crew hygiene and food techniques). In addition to the life support equipment, a number of crew tests simulated specific problems of space flight. Five days later, however, the simulated mission was halted because of a faulty reactor tank.
1963 July 16 - -
Cosmonauts brainstorm improvements Nation: USSR. Flight: Vostok 6. Gagarin is in the hospital to have his inflamed tonsils removed. A brainstorming session is held with the flown cosmonauts to identify problems encountered in flight and necessary improvements to training and flight operations to prevent them from reoccurring. The Military Soviet meets but the issue of Odintsev is not taken up -- his defenders in the hierarchy manage to suppress discussion of his removal.
References: 376.
1963 July 16 - Launch Site: Vandenberg. Launch Complex: 395-A2. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I SM-24. -
Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,000 km (600 mi). References: 2.
1963 July 16-August 15 - -
Testing of the launch escape system pitch control motor Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. North American reported that Lockheed Propulsion Company had successfully completed development testing of the launch escape system pitch control motor. References: 16.
1963 July 17 - -
Rudenko meets Odintsev Nation: USSR. Rudenko meets Odintsev but does not give him the word of his removal directly. The decision will wreck Odintsev's career - his next assignment would have been command of an Air Army. Odintsev fretted over the number of stars on his uniform and fawned over academics -- he never looked after his own people, which would have prevented things coming to this.
References: 376.
1963 July 17 - Launch Site: Cape Canaveral. Launch Complex: LC21/1. Launch Pad: LC21/pad?. Launch Vehicle: Mace. LV Configuration: Mace 59-4981. -
Test mission Nation: USA. Agency: USAF 4505MTW. Apogee: 12 km (7 mi). References: 2.
1963 July 18 - -
Pratt and Whitney to develop fuel cells for the Apollo LEM Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Grumman selected Pratt and Whitney to develop fuel cells for the LEM. Current LEM design called for three cells, supplemented by a battery for power during peak consumption beyond what the cells could deliver. Grumman and Pratt and Whitney completed contract negotiations on August 27, and MSC issued a letter go-ahead on September 5. Including fees and royalties, the contract was worth $9.411 million.
References: 16.
1963 July 18 - 18:07 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 1-38-61. -
X-15A VO Stability test Nation: USA. Agency: NASA/USAF. Apogee: 31 km (19 mi). Maximum Speed - 6315 kph. Maximum Altitude - 31940 m. References: 2.
1963 July 19 - -
Marquardt begins development of the Apollo LEM reaction control thrusters Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Grumman directed the Marquardt Corporation to begin development of the LEM reaction control system thrusters. Negotiations had begun on March 11 on the definitive subcontract, a cost-plus-incentive-fee type with a total estimated cost of $10,871,186. References: 16.
1963 July 19 - -
Cosmonaut tour plans through December 1963. Nation: USSR. Flight: Vostok 6, Vostok 5. Cosmonaut tour plans are firmed up for September-December 1963.. Tereshkova and Bykovskiy are to be given a gruelling schedule, having to visit Bulgaria, Mongolia, Italy, Switzerland, Norway, Mexico, India, Ghana, and Indonesia. References: 376.
1963 July 19 - 00:00 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena D. LV Configuration: Thor Agena D 388 / Agena D 1412. -
KH-4 9057 Nation: USA. Payload: KH-4 s/n 9057 / Agena D 1412. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: NRO/CIA. Perigee: 197 km (122 mi). Apogee: 382 km (237 mi). Inclination: 82.90 deg. Period: 90.40 min. COSPAR: 1963-029A. USAF Sat Cat: 621. Decay Date: 1963-08-13. KH-4. Best mission to date. References: 2, 6.
1963 July 19 - 01:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-27. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 July 19 - 03:51 GMT - Launch Site: Vandenberg. Launch Complex: SLC3E. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 75D / Agena B S01 1207. -
Midas 9 Nation: USA. Payload: Midas / Agena TV 1207. Mass: 2,000 kg (4,400 lb). Class: Early Warning. Spacecraft: Midas. Agency: USAF. Perigee: 3,676 km (2,284 mi). Apogee: 3,726 km (2,315 mi). Inclination: 88.40 deg. Period: 167.90 min. COSPAR: 1963-030A. USAF Sat Cat: 622. Missile Defense Alarm System. Did not eject ERS 10 subsatellite. References: 2, 6, 171, 172, 278.
-
TRS 4 Nation: USA. Payload: ERS 9. Mass: 2.00 kg (4.40 lb). Class: Technology. Spacecraft: TRS. Agency: USAF. Perigee: 3,661 km (2,274 mi). Apogee: 3,736 km (2,321 mi). Inclination: 88.40 deg. Period: 167.80 min. COSPAR: 1963-030B. USAF Sat Cat: 635. Radiation damage data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
-
Dash 2 Nation: USA. Class: Technology. Type: Military. Spacecraft: Dash. Agency: USAF. Perigee: 3,573 km (2,220 mi). Apogee: 3,839 km (2,385 mi). Inclination: 88.50 deg. Period: 168.00 min. COSPAR: 1963-030D. USAF Sat Cat: 624. Decay Date: 1971-04-12. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
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TRS 10 Nation: USA. Payload: ERS 10. Class: Earth. Type: Magnetosphere. Spacecraft: ERS. Agency: USAF AFSC. COSPAR: 1963-030xx. References: 2, 279.
1963 July 19 - 05:30 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.37GG. -
Ultraviolet spectrograph Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 185 km (114 mi). References: 2.
1963 July 19 - 18:20 GMT - Launch Site: Smith Ranch Lake DZ. Launch Complex: -. Launch Pad: 39.3 N x 117.5 W. Launch Vehicle: X-15. LV Configuration: X-15 3-21-32. -
X-15A VO,UVP,IR,HS,Balloon Test/Technology/Ultraviolet Astronomy mission Nation: USA. Agency: NASA/USAF. Apogee: 106 km (65 mi). Maximum Speed - 5969 kph. Maximum Altitude - 106010 m. Astronaut wings flight. 80 cm diameter balloon dragged on 30 m line to measure air density. First X-15 astronaut flight (FAI definition); fourth astronaut wings flight (USAF definition). References: 2.
1963 July 20 - -
Scientific objectives for spaceflights in 1964 Nation: USSR. Keldysh issues a letter listing the scientific objectives for spaceflights in 1964: - Photograph on marked film the earth and its atmosphere, the surfaces of the moon and planets,
- Observe the zodiacal light via photometer
- Conduct spectrographic analysis of the earth's atmosphere in the 3000 to 3600 Angstrom range
- Conduct ultraviolet spectroscopy of the sky at 304 and 60 Angstroms
- Map the infrared radiation of the earth from space, especially of the polar regions
References: 376.
1963 July 20 - 05:44 GMT - Launch Site: Wallops Island. Launch Complex: LA3. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-3A. LV Configuration: Scout X-3A S110. FAILURE: Failure. -
Reentry 3 re-entry vehicle test flight Nation: USA. Agency: NASA. Apogee: 2.00 km (1.20 mi). NASA launched a Scout rocket with a nose cone of experimental heatshield material from Wallops Island, Va. The rocket was intentionally destroyed when it deviated from its course a few seconds after liftoff. The nose cone had been expected to reenter the atmosphere at 27,934 kilometers (18,600 miles) per hour to test the material's thermal performance under heating loads near those of a lunar reentry.
References: 2.
1963 July 20 - 15:18 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.77GS. -
OSO B spectrometer Solar ultraviolet / eclipse mission Nation: USA. Agency: NASA. Apogee: 213 km (132 mi). References: 2.
1963 July 20 - 21:03 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.91CI. -
Operation Probe High Ionosphere / eclipse mission Nation: USA. Agency: NASA. Apogee: 196 km (121 mi). References: 2.
1963 July 20 - 21:05 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5A. LV Configuration: Black Brant VA AB17.199. -
Operation Probe High Eclipse mission Nation: USA. Agency: USAF. Apogee: 143 km (88 mi). References: 2.
1963 July 20 - 21:13 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.92CI. -
Opn Probe High Ionosphere / eclipse / solar x-rays mission Nation: USA. Agency: NASA. Apogee: 199 km (123 mi). References: 2.
1963 July 20 - 21:40 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.93CI. -
Opn Probe High Ionosphere / eclipse / solar x-rays mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1963 July 20 - 21:54 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 300A. LV Configuration: Aerobee 300A NASA 06.08GA. -
Thermosphere Probe 3 Aeronomy / eclipse mission Nation: USA. Agency: NASA. Apogee: 338 km (210 mi). References: 2.
1963 July 20 - 22:10 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.94CI. -
Opn Probe High Ionosphere / eclipse / solar x-rays mission Nation: USA. Agency: NASA. Apogee: 192 km (119 mi). References: 2.
1963 July 22 - -
Conference on space cabin ecology. Nation: USSR. Spacecraft: TMK-1. Keldysh, Korolev, Voronin, and Kamanin attend a conference on space cabin ecology. Presentations are made by IAKM, OKB-124, the Biology Institute, and the Physiology Institute. In two to three years the USSR expects to orbit spacecraft of 78 to 80 tonnes, which will be assembled in earth orbit to produce larger spacecraft. These will not only fly around the moon, but also be used to fly to Venus, Mars, and other planets. Although it will take years, many technical problems have to be solved before such a spacecraft can be built. How to shield the crew from radiation? How best to regenerate the air? How to recycle the water? Can the crew survive for long flights in zero-G, or must some form of artificial gravity be provided? If so, what is the best method? How can the psychological health of the crew best be maintained on long flights? It is reported that a lot of test stand work has been completed and is underway on closed ecological systems for recycling the air and water. One kilogram of chlorella algae can produce 27 kg of oxygen per day. Since each man will require 25 kg of oxygen per day, 2 kg of chlorella per crew member will be adequate. Therefore the problem of recycling the cabin atmosphere is considered already solved. Food requirements per crew member are 2.5 to 3.0 kg/day, or about one tonne per year. It is expected that in two to three years development will be complete of a system that will recycle 80% of the food. A 150 kg device will produce 400 to 600 g of food per day, or 100 to 200 kg per year.
References: 376.
1963 July 22 - -
Johnson requests statement on the importance to national security of a space station. Nation: USA. Spacecraft: Dynasoar, MOL. Vice President Lyndon B. Johnson requested the Secretary of the Defense to prepare a statement on the importance to national security of a space station.
1963 July 23 - -
Hamilton Standard began development of the ECS for the Apollo LEM Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Grumman authorized Hamilton Standard to begin development of the environmental control system (ECS) for the LEM. The cost-plus-incentive-fee contract was valued at $8,371,465. The parts of the ECS to be supplied by Hamilton Standard were specified by Grumman.
References: 16.
1963 July 23 - -
George E Mueller named NASA Deputy Associate Administrator Nation: USA. Program: Apollo. George E. Mueller, Vice President for Research and Development of Space Technology Laboratories, was named NASA Deputy Associate Administrator for Manned Space Flight to succeed D. Brainerd Holmes, effective September 1. References: 16.
1963 July 23 - 06:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.29GG. -
Ultraviolet spectrograph Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 177 km (109 mi). References: 2.
1963 July 24 - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 432. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1963 July 24 - 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 July 25 - -
Gagarin released from the hospital Nation: USSR. Gagarin is released from the hospital after his tonsillectomy. References: 376.
1963 July 25 - 14:15 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NB3.124. -
Solar X-rays Spectrum 2 Solar x-ray mission Nation: USA. Agency: NRL. Apogee: 200 km (120 mi). References: 2.
1963 July 25 - 22:38 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Exos. LV Configuration: Exos CRL AC13.831. -
Refractive Index Ionosphere mission Nation: USA. Agency: USAF. Apogee: 623 km (387 mi). References: 2.
1963 July 26 - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-33. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 July 26 - 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 test Nation: USA. Agency: USA. Apogee: 200 km (120 mi). References: 2.
1963 July 26 - 14:33 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Delta B. LV Configuration: Thor Delta B 370/D20. -
Syncom 2 Nation: USA. Mass: 39 kg (85 lb). Class: Technology. Type: Comsat. Spacecraft: Syncom. Agency: NASA GSF. Perigee: 35,891 km (22,301 mi). Apogee: 35,891 km (22,301 mi). Inclination: 32.70 deg. Period: 1,441.50 min. COSPAR: 1963-031A. USAF Sat Cat: 634. Completed Operations Date: 1969-04-01. Experimental commsat; 1st geosynchronous satellite. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit at 55 deg W in 1963; 26 deg W in 1965. Last known longitude (19 July 1995) 68.47 deg E drifting at 0.089 deg W per day.
References: 2, 6.
1963 July 26 - 19:19 GMT - Launch Site: Vandenberg. Launch Complex: OSTF1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 24E. FAILURE: Failure. -
Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 300 km (180 mi). References: 2.
1963 July 26 - 21:19 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5A. LV Configuration: Black Brant VA AC17.61. -
D region e density Aurora / ionosphere mission Aurora / ionosphere mission Nation: USA. Agency: USAF. Apogee: 143 km (88 mi). References: 2.
1963 July 27 - -
Korolev on future manned space flight plans. Nation: USSR. Flight: Vostok 7, Vostok 8, Vostok 9, Vostok 10. Another meeting is held with Korolev on future manned space flight plans. The same plans are presented as have been discussed for over a year - one animal flight, three manned flights for 10 days / to 1000 km. This issue must be resolved. Soyuz will not fly before 1965 - therefore Vostok must be flown or there will no Soviet manned spaceflights in 1964. In reality Soyuz is likely to be delayed, and 6 to 8 Vostoks are needed, not just 4. Equipment to be tested on the flights included soft landing equipment, a back-up retrofire engine, long-range communications systems, and scientific experiments. The physicians are too conservative - zero-G is obviously not as big an issue as thought. There should be nothing to prevent flight of non-pilot passengers. Korolev points out that if the cosmonaut is consumed by fear, or if any serious problem arises, as long as you can survive for an hour an emergency return to earth can be made. Within an hour the passenger will be in Cuba or Vladivostok. Kamanin would like Gagarin to be appointed next head of the cosmonaut centre, but this is opposed by Rudnev and Vershinin. Tereshkova has talked to Khrushchev - he's now supporting award of a Hero of the Soviet Union medal to Nikitin.
References: 376.
1963 July 27 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 514. -
Demonstration and shakedown operations launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1963 July 27 - Launch Site: Baikonur. Launch Complex: LC41/15. 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 July 27 - 00:10 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun K-63-1. -
Grenades Aeronomy mission Nation: Sweden. Agency: RTG. Apogee: 126 km (78 mi). References: 2.
1963 July 29 - 23:28 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun K-63-2. -
Grenades Aeronomy mission Nation: Sweden. Agency: RTG. Apogee: 128 km (79 mi). References: 2.
1963 July 30 -
1963 July 30 - 16:16 GMT - Launch Site: Cape Canaveral. Launch Complex: LC18A. Launch Pad: LC18A. Launch Vehicle: Scout. Model: Blue Scout Jr. LV Configuration: Blue Scout Jr 22-1/AD-622. -
OAR 22-1 / AFCRL-1 / 21 Plasma / radio astronomy mission Nation: USA. Agency: USAF. Apogee: 11,100 km (6,800 mi). References: 2.
1963 July 30 - 18:36 GMT - Launch Site: Vandenberg. Launch Complex: 576C. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 70E. -
Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,600 km (900 mi). References: 2.
1963 July 31 - 00:00 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 382 / Agena D 1167. -
KH 4A-07 Nation: USA. Payload: KH-6 s/n 8003 / Agena D 1167. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-6. Agency: NRO/CIA. Perigee: 152 km (94 mi). Apogee: 455 km (282 mi). Inclination: 74.90 deg. Period: 90.60 min. COSPAR: 1963-032A. USAF Sat Cat: 626. Decay Date: 1963-08-12. KH-6. Third and final KH-6 mission (LANYARD). Mission was successful but image quality was poor. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
1963 July 31 - 20:52 GMT - Launch Site: Vandenberg. Launch Complex: 576B1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 143D. -
ST COOL WATER I test Nation: USA. Agency: USAF SAC. Apogee: 1,000 km (600 mi). References: 2.
1963 August 1 - 08:06 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NC3.?. -
Bennett Mass Spec 2 Aeronomy mission Nation: USA. Agency: NRL. Apogee: 232 km (144 mi). References: 2.
1963 August 1 - 23:27 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun K-63-3. -
Grenades Aeronomy mission Nation: Sweden. Agency: RTG. Apogee: 126 km (78 mi). References: 2.
1963 August 2 - Launch Vehicle: Saturn V. -
Grumman to design the LEM to have a thrusting capability with the Apollo CSM attached Nation: USA. Program: Apollo. Spacecraft: Apollo LM. North American asked MSC if Grumman was designing the LEM to have a thrusting capability with the CSM attached and, if not, did NASA intend to require the additional effort by Grumman to provide this capability. North American had been proceeding on the assumption that, should the service propulsion system (SPS) fail during translunar flight, the LEM would make any course corrections needed to ensure a safe return trajectory.
Additional Details: Grumman to design the LEM to have a thrusting capability with the Apollo CSM attached. References: 16.
1963 August 2 - -
No further Soviet manned flights in 1963 Nation: USSR. Flight: Vostok 7. It is clear that there may be no Soviet manned flights in 1963, and certainly not in the spring. It is possible the unmanned biosat Vostok will be flown in the second half of 1963. Korolev's plate is full with other work -- Soyuz development, several Zenit reconnaissance satellite launches, lots of Luniks. Meanwhile Kamanin is completely occupied with cosmonaut tours and publicity. Over 200,000 cosmonaut fan letters have been received -- they can't handle them all, a special unit will have to be created just to handle the mail. The KGB has assigned Yevgeniya Pavlovna Kassirova to accompany Tereshkova on her travels. She is a good choice, has foreign travel experience and excellent English.
References: 376.
1963 August 2 - Launch Site: Point Mugu. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sparoair. Model: Sparoair I. -
Ultraviolet astronomy mission Nation: USA. Agency: USN NMC. Apogee: 107 km (66 mi). References: 2.
1963 August 2 - 21:43 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sergeant. Model: Shotput. LV Configuration: Shotput 7. -
San Marco Satellite test Nation: USA. Agency: NASA. Apogee: 294 km (182 mi). References: 2.
1963 August 2 - 23:33 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.75UA. -
Density Aeronomy mission Nation: USA. Agency: NASA. Apogee: 151 km (93 mi). References: 2.
1963 August 5 - Launch Vehicle: Saturn I. -
First static firing test of Saturn S-IV stage for SA-5 Nation: USA. Program: Apollo. In what was to have been an acceptance test, the Douglas Aircraft Company static fired the first Saturn S-IV flight stage at Sacramento, Calif. An indication of fire in the engine area forced technicians to shut down the stage after little more than one minute's firing. A week later the acceptance test was repeated, this time without incident, when the vehicle was fired for over seven minutes. (The stage became part of the SA-5 launch vehicle, the first complete Saturn I to fly.)
References: 16.
1963 August 5 - Launch Site: Fort Wingate. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 2033. -
Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Successful missile test. Missed aimpoint by 216 m. References: 2.
1963 August 5 - 16:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 433. FAILURE: Failure. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 100 km (60 mi). References: 2.
1963 August 6 - 06:00 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. -
Cosmos 19 Nation: USSR. Program: DS. Payload: DS-P1 s/n 3. Mass: 355 kg (782 lb). Class: Military. Type: Target. Spacecraft: DS-P1. Agency: MO SSSR. Perigee: 267 km (165 mi). Apogee: 497 km (308 mi). Inclination: 49.00 deg. Period: 92.10 min. COSPAR: 1963-033A. USAF Sat Cat: 632. Completed Operations Date: 1964-03-29. Decay Date: 1964-03-30. Prototype ABM radar target; supported developmental experiments for ABM systems. References: 2, 6, 99.
1963 August 7 - 22:29 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun K-63-4. -
Grenades Aeronomy mission Nation: Sweden. Agency: RTG. Apogee: 130 km (80 mi). References: 2.
1963 August 8 - 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 August 8 - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 520. -
Demonstration and shakedown operations launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi). References: 2.
1963 August 9 - -
McNamara sees necessity of multi-manned orbital flights of long duration. Nation: USA. Spacecraft: Dynasoar, MOL. In his reply to the Vice President, Secretary McNamara stressed the necessity of multi-manned orbital flights of long duration.
1963 August 9 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-210. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 August 9 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-209. -
Operational Test - Flight over 65 minutes Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 August 10 - 03:17 GMT - Launch Site: Niijima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Lambda. Model: LS-A. LV Configuration: LS-A Sustainer. -
Test mission Nation: Japan. Agency: STA. Apogee: 50 km (31 mi). References: 2.
1963 August 10 - 04:58 GMT - Launch Site: Niijima. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-A. LV Configuration: S-A1. -
Test mission Nation: Japan. Agency: STA. Apogee: 50 km (31 mi). References: 2.
1963 August 11 - -
Kamanin picks up a new Volga automobile. Nation: USSR. Flight: Vostok 6, Vostok 7, Vostok 8, Vostok 9, Vostok 10. Kamanin picks up a new Volga automobile. It cost him 5513 roubles, but one door doesn't fit and the trunk is scarred with excess hardened resin. Sukarno has asked for Tereshkova and Bykovskiy to visit Indonesia for two weeks in August, but this is impossible. In a three hour meeting Korolev goes over his future flight plans for Vostok. The first flight will be unmanned, with a biological payload, in February or March 1964. The flight is to last 10 or 11 days and take the specimens up to 600 to 1000 km altitude, into the lower reaches of the Van Allen radiation belts. This will be followed by three cosmonaut flights of ten days with significant military and scientific experiments. A new ground control system will be installed and tested to handle all in-flight emergencies. A new autonomous on-board navigation system will be flight tested. Korolev wants the military to take over conduct of future Vostok flights - they are taking up to much of his time and nerves. He has told this repeated to Khrushchev and Brezhnev without result. Meanwhile Kamanin lobbies within the military hierarchy for the removal of Odintsev. It is decided that the matter will be taken up at the next meeting of the Military Soviet.
References: 376.
1963 August 13 - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-36. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 August 13 - 04:59 GMT - Launch Site: Baikonur. Launch Complex: LC41/15. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Combat training launch Nation: USSR. Agency: RVSN. Apogee: 757 km (470 mi). References: 2.
1963 August 15 - Launch Site: Vandenberg. Launch Complex: 395-A1. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I SM-7. -
Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,000 km (600 mi). References: 2.
1963 August 15 - Launch Site: White Sands. Launch Complex: LC38. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3. -
K-26 Titan Intercept Nation: USA. Agency: USA. Apogee: 200 km (120 mi). References: 2.
1963 August 17 - 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 August 17 - 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 August 17 - 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 August 17 - 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 August 17 - 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 August 17 - 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 August 17 - September 14 - -
NASA / DOD agreement to coordinate all advanced space exploration studies and manned orbital research station programs. Nation: USA. NASA and the DOD concluded a joint agreement to coordinate all advanced space exploration studies and any actual programs undertaken in the area of a manned orbital research station. The two agencies agreed that, to the greatest extent possible, future requirements in this area should be encompassed in a single project.
1963 August 19 - Launch Site: Fort Wingate. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 2008. -
Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Successful missile test. Missed aimpoint by 267 m. References: 2.
1963 August 20 - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-37. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 August 20 - Launch Site: Baikonur. Launch Complex: LC60/8. 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 August 21 - 23:23 GMT - Launch Site: Cape Canaveral. Launch Complex: LC15. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-24. -
Research and development / Pod T-202 test / plume study mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Titan II development flight N-24 was launched from the Atlantic Missile Range. This was the first of five flight tests in the Gemini malfunction detection system (MDS) piggyback series. All MDS parameters were lost 81 seconds after liftoff because of a short circuit in the MDS. Operation in the second flight (N-25 on November 1) was normal except for two minor instrumentation problems. Three more test flights (N-29 on December 12, 1963; N-31 on January 15, 1964; and N-33 on March 23, 1964) verified the performance of the Gemini MDS under actual conditions of flight environment and engine operation.
References: 2.
1963 August 22 - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. FAILURE: First stage failed. -
DS-A1 s/n 3 Nation: USSR. Program: DS. Payload: DS-A1. Class: Technology. Type: Navigation. Spacecraft: DS-A1. Agency: RVSN. COSPAR: F630822A. 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 August 22 - 18:05 GMT - Launch Site: Smith Ranch Lake DZ. Launch Complex: -. Launch Pad: 39.3 N x 117.5 W. Launch Vehicle: X-15. LV Configuration: X-15 3-22-36. -
X-15A VO,Spectrom,Photom Test/Aeronomy mission Nation: USA. Agency: NASA/USAF. Apogee: 107 km (66 mi). Unofficial world altitude record. Maximum Speed - 6105 kph. Maximum Altitude - 107960 m. Second X-15 astronaut flight (FAI definition); fifth astronaut wings flight (USAF definition). References: 2.
1963 August 23 - 17:01 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-208. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 August 23 - 17:41 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-211. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 August 24 - Launch Site: Kwajalein. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3. -
K-28 Atlas Intercept Nation: USA. Agency: USA. Apogee: 200 km (120 mi). References: 2.
1963 August 24 - 02:00 GMT - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: -. Launch Vehicle: Lambda. Model: Lambda 2. LV Configuration: Lambda 2 L-2-1. FAILURE: Failure. -
Ionosphere / test Nation: Japan. Agency: ISAS. Apogee: 51 km (31 mi). References: 2.
1963 August 24 - 09:50 GMT - Launch Site: Vandenberg. Launch Complex: OSTF1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 72E. -
NTMP/OT DASO test Nation: USA. Agency: USAF SAC. Apogee: 1,600 km (900 mi). References: 2.
1963 August 25 - 00:30 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 377 / Agena D 1162. -
KH-4A 1001 Nation: USA. Payload: KH-4A s/n 1001 / Agena D 1162. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 161 km (100 mi). Apogee: 320 km (190 mi). Inclination: 75.00 deg. Period: 89.40 min. COSPAR: 1963-034A. USAF Sat Cat: 636. Decay Date: 1963-09-12. KH-4A. First mission of KH-4A. Some film was fogged. Two buckets but 1001-2 was never recovered. References: 2, 6.
1963 August 27 - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 435. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1963 August 28 - 16:00 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Little Joe II. Model: Little Joe II 6-1-0. LV Configuration: Little Joe II-6-1-0 LJII-1 (12-50-1). -
QTV Spacecraft test Nation: USA. Agency: NASA. Apogee: 8.00 km (4.90 mi). The Little Joe II qualification test vehicle was launched from White Sands Missile Range, N Mexico. Its objectives were to prove the Little Joe's capability as an Apollo spacecraft test vehicle and to determine base pressures and heating on the missile. These aims were achieved. The lone failure was a malfunction in the destruct system.
References: 2.
1963 August 28 - 23:10 GMT - Launch Site: Vandenberg. Launch Complex: 576B3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 142D. -
ST COOL WATER II test Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1963 August 29 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 625. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1963 August 29 - 20:31 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2 Agena D. LV Configuration: Thor SLV-2 Agena D 394 / Agena D 1169. -
KH-4 9033 Nation: USA. Payload: KH-4 s/n 9033 & Lampo / Agena D 1169. Mass: 1,000 kg (2,200 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: NRO/CIA. Perigee: 292 km (181 mi). Apogee: 324 km (201 mi). Inclination: 81.90 deg. Period: 90.80 min. COSPAR: 1963-035A. USAF Sat Cat: 637. Decay Date: 1963-11-07. KH-5; deployed ELINT subsatellite. Considered to be best mission to date in Argon program. References: 2, 6.
-
LAMPO Nation: USA. Payload: 0.1 Square Meter Target. Class: Sigint. Spacecraft: LAMPO. Agency: USAF. Perigee: 315 km (195 mi). Apogee: 422 km (262 mi). Inclination: 81.90 deg. Period: 92.00 min. COSPAR: 1963-035B. USAF Sat Cat: 638. Decay Date: 1963-09-29. Radar monitoring. Not identified as a subsatellite ferret by McDowell. References: 2, 6, 172.
1963 August 30 -
1963 August 30 - -
Enabling decree for Plesetsk cosmodrome. Nation: USSR. Decree 'On formation of NIIP-53 at Angara' was issued. References: 474.
1963 August 30 - -
Washington-to-Moscow hot line Nation: USSR. Washington-to-Moscow hot line communications link opens, designed to reduce risk of accidental war
1963 August 30 - -
Study for a military, orbiting, space station. Nation: USA. Spacecraft: Dynasoar, MOL. The Director of Defense for Research and Engineering approved a study program for a military, orbiting, space station.
1963 August 30 - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-38. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1963 August 30 - Launch Site: Vandenberg. Launch Complex: 395-A3. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I SM-56. -
Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,000 km (600 mi). References: 2.
1963 August 30 - 06:30 GMT - Launch Site: Baikonur. Launch Complex: LC41/3. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
T Nation: USSR. Agency: RVSN. Apogee: 754 km (468 mi). References: 2.
1963 August 31 - -
Parasail and landing rocket system considered to enable the Gemini spacecraft to make land landings. Nation: USA. Program: Gemini. Spacecraft: Gemini. Gemini Project Office (GPO) reported that it was investigating the use of a parasail and landing rocket system to enable the Gemini spacecraft to make land landings. Major system components were the parasail, drogue parachute, retrorocket, control system, and landing rocket. Unlike the conventional parachute, the parasail was capable of controlled gliding and turning. Landing rockets, fired just before touchdown, reduced the spacecraft terminate rate of descent to between 8 and 11 feet per second. Research and development testing was being conducted by the Landing and Impact System Section of Systems Evaluation and Development Division at Manned Spacecraft Center, while McDonnell had just completed a limited study of the advantages and disadvantages, including time required, of incorporating the new landing system on the spacecraft. GPO briefed NASA Headquarters on the system September 6, when it was decided that no further action would be taken on the parasail.
1963 August -
1963 September 1 - Launch Site: Baikonur. Launch Complex: LC110L. Launch Pad: -. Launch Vehicle: N1. -
Construction begins of N1 launch complex Nation: USSR. Program: Lunar L3. References: 96.
1963 September 1 - Launch Site: Sary Shagan. Launch Complex: LC6. Launch Pad: -. Launch Vehicle: A-35. Model: A-350Zh. LV Configuration: A-350Zh 6TYa F1. -
Test mission Nation: USSR. Agency: PRO. Apogee: 100 km (60 mi). References: 2.
1963 September - -
Korolev earth orbit rendezvous L3 manned lunar lander design. Nation: USSR. Spacecraft: L3-1963. This L3 design was a 200 tonne direct-lander requiring three launches of his giant N1 rocket and assembled in low earth orbit.
1963 September 1-7 - -
Design of control panel for the Apollo CM was 90 percent complete Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. MSC reported that design of the control and displays panel for the CM was about 90 percent complete. North American was expected to release the design by September 20. Qualification testing of the panels would begin around December 1. References: 16.
1963 September 3 - 22:36 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AD3.374. -
Mass spectrometer Aeronomy mission Nation: USA. Agency: USAF. Apogee: 288 km (178 mi). References: 2.
1963 September 4 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1963 September 4 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1963 September 4 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1963 September 4 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1963 September 4 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1963 September 4 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1963 September 4 - Launch Site: Baikonur. Launch Complex: LC41/3. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
T Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1963 September 4 - 13:11 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.91GE. -
CR nuclei Cosmic rays mission Nation: USA. Agency: NASA. Apogee: 228 km (141 mi). References: 2.
1963 September 5 - Launch Site: Barbados. Launch Complex: HARP. Launch Pad: -. Launch Vehicle: Martlet. Model: Martlet 3. -
Test mission Nation: Canada. Agency: HARP. Apogee: 100 km (60 mi). The Martlet 3A gun-launched rocket program began in the spring of 1963 with test flights beginning in September. Early Martlet 3A test flights were less then successful. At launch loads of 5000-6000 g’s the rocket motor fuel grain would fail.The Martlet 3A set a world record as the largest rocket launched from a gun.
References: 2.
1963 September 5 - 03:41 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 5C. LV Configuration: Skylark-5C SL87. -
Test mission Nation: Australia. Agency: WRE/RAE. Apogee: 214 km (132 mi). References: 2.
1963 September 6 - -
Apollo CM boilerplate destroyed during tests Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. At El Centro, Calif., CM boilerplate (BP) 3, a parachute test vehicle, was destroyed during tests simulating the new BP-6 configuration (without strakes or apex cover). Drogue parachute descent, disconnect, and pilot mortar fire appeared normal. However, one pilot parachute was cut by contact with the vehicle and its main parachute did not deploy. Because of harness damage, the remaining two main parachutes failed while reefed. Investigation of the BP-3 failure resulting in rigging and design changes on BP-6 and BP-19.
References: 16.
1963 September 6 - Launch Vehicle: Titan. Model: Titan 2. -
Department of Defense approved the Titan II Augmented Engine Improvement Program. Nation: USA. On November 15, Aerojet-General received an Air Force contract to develop and test new engine components to correct weak and potentially dangerous problem areas of engine design. Aerojet-General had already initiated the development effort on September 30. The goal was to enhance engine reliability by a complete redesign rather than resort to piecemeal fixes as problems came up. While the primary goal was not achieved, the program did yield several side benefits, including the correction of several minor design deficiencies, the improvement of welding techniques, and the development of better assembly procedures.
1963 September 6 - -
Tereshkova accused of a scandal in Gorkiy. Nation: USSR. Flight: Vostok 6. The militia claims that Tereshkova was drunk and created a scandal with a militia officer in Gorkiy. She categorically denies being drunk, but does admit to having a confrontation with a militia captain. References: 376.
1963 September 6 - 19:30 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena D. LV Configuration: Atlas Agena D 212D / Agena D S01A 4701. -
KH 7-02 Nation: USA. Payload: KH-7 no. 2. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-7. Agency: NRO/USAF. Perigee: 171 km (106 mi). Apogee: 243 km (150 mi). Inclination: 94.40 deg. Period: 88.70 min. COSPAR: 1963-036A. USAF Sat Cat: 641. Decay Date: 1963-09-13. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6, 278.
1963 September 6 - 21:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.22US. -
OSO B experiment Solar mission Nation: USA. Agency: NASA. Apogee: 222 km (137 mi). References: 2.
1963 September 6 - 21:59 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 63D. FAILURE: Failure. -
ST COOL WATER III test Nation: USA. Agency: USAF SAC. Apogee: 200 km (120 mi). References: 2.
1963 September 7 - -
Tereshkova and Bykovskiy begin an eight day tour of Bulgaria. Nation: USSR. Flight: Vostok 6, Vostok 5. References: 376.
1963 September 9 - 16:02 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.06UE. -
Electrojet Magnetospheric mission Nation: USA. Agency: NASA. Apogee: 169 km (105 mi). References: 2.
1963 September 10 - Launch Site: Fort Wingate. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 2015. FAILURE: Control system malfunction immediately prior to impact. -
Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Missile test failure. Missed aimpoint by 4,393 m. References: 2.
1963 September 10 - 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 September 11 - 14:24 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.32NP. -
LeRC LH2 test Technology test Nation: USA. Agency: NASA. Apogee: 165 km (102 mi). References: 2.
1963 September 11 - 21:00 GMT - Launch Site: Vandenberg. Launch Complex: 576B1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 84D. FAILURE: Failure. -
ST COOL WATER IV test Nation: USA. Agency: USAF SAC. Apogee: 1,700 km (1,000 mi). References: 2.
1963 September 12 - -
Unmanned lunar landing spacecraft to be sterilized Nation: USA. Program: Apollo. Spacecraft: Surveyor. NASA announced that, in the future, unmanned lunar landing spacecraft e.g., Rangers and Surveyors) will be assembled in "clean rooms" and treated with germ-killing substances to reduce the number of microbes on exposed surfaces. These sterilization procedures, less stringent than earlier methods, were intended to prevent contamination of the lunar surface and, at the same time, avoid damage to sensitive electronic components. Heat sterilization was suspected as one of the reasons for the failure of Ranger spacecraft.
References: 16.
1963 September 12 - -
Gemini, Apollo, and X-20 studied for military space missions. Nation: USA. Spacecraft: Dynasoar, MOL, Gemini, Apollo CSM. The President's Scientific Advisory Committee requested a briefing from the Air Force on possible military space missions, biomedical experiments to be performed in space, and the capability of Gemini, Apollo, and the X-20 vehicles to execute these requirements.
1963 September 12 - 06:20 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache Ferdinand 4. -
Ferdinand 4 Ionosphere / plasma / solar mission Nation: Norway. Agency: NDRE?. Apogee: 136 km (84 mi). References: 2.
1963 September 14 - Launch Vehicle: Titan. Model: Titan 2. -
Gemini Project Office reported a delay of about three weeks in the battery qualification program. Nation: USA. McDonnell had sent a team to investigate the problem of high porosity welds in titanium battery cases. Another problem had turned up with the batteries in prequalification vibration test. The batteries vibrated excessively, although they did not fail electrically; the vibration's amplification factor was apparently low enough to be remedied by potting.
1963 September 16 - -
Enabling decree for Plesetsk cosmodrome. Nation: USSR. Decree 999-347 'On creation or the space and missile cosmodrome at NIIP-53 at Mirniy/Plesetsk' was issued. References: 474.
1963 September 16-18 - -
Inspection of first Apollo LEM ascent stage mockup Nation: USA. Program: Apollo. Spacecraft: Apollo LM. NASA representatives held a formal review of Grumman's LEM M-1 mockup, a full-scale representation of the LEM's crew compartment. MSC decided that (1) the window shape (triangular) and visibility were satisfactory; (2) a standing position for the crew was approved, although, in general, it was believed that restraints restricted crew mobility; (3) the controllers were positioned too low and lacked suitable arm support for fine control; and (4) crew station arrangement was generally acceptable, although specific details required further study.
References: 16.
1963 September 17 - -
Cosmonaut training group formed for planned 1964 Vostok flights Nation: USSR. Spacecraft: Vostok. Flight: Vostok 7, Vostok 8, Vostok 9, Vostok 10. Belyaev, Komarov, Shonin, Khrunov, Zaikin, Gorbatko, Volynov, and Leonov are assigned. References: 376.
1963 September 17 - Launch Site: Vandenberg. Launch Complex: 395-A2. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I SM-83. -
Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,000 km (600 mi). References: 2.
1963 September 18 - -
AiResearch awarded contract for the Apollo CM environmental system Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The AiResearch Manufacturing Company announced that it had been awarded a $20 million definitive contract for the CM environmental system. (AiResearch had been developing the system under a letter contract since 1961. References: 16.
1963 September 18 - 09:39 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2F. LV Configuration: Thor DSV-2F 232. -
ASSET 1 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 56 km (34 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. Booster flew to peak altitude of 62 km, then pitched down, driving the spacecraft to separation at 59 km and 4,906 m/s. The spacecraft was sited under its parachute in the recovery zone at Ascension Island, but the flotation bag broke and it sank into the Atlantic.
References: 2.
1963 September 20 - -
President Kennedy suggested Russian-American cooperation in space Nation: USA. Program: Apollo. President John F. Kennedy, during an address before the United Nations General Assembly, suggested the possibility of Russian-American "cooperation" in space. Though not proposing any specific program, Kennedy stated that, "in a field where the United States and the Soviet Union have a special capacity - the field of space - there is room for new cooperation, for further joint efforts in the regulation and exploration of space. I include among these possibilities," he said, "a joint expedition to the moon. . . . Surely we should explore whether the scientists and astronauts of our two countries - indeed, of all the world - cannot work together in the conquest of space, sending some day in this decade to the moon, not the representatives of a single nation, but the representatives of all humanity."
Additional Details: President Kennedy suggested Russian-American cooperation in space. References: 16.
1963 September 20 - 15:45 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NE3.151. -
SX solar spectrum Solar extreme ultraviolet mission Nation: USA. Agency: NRL. Apogee: 208 km (129 mi). References: 2.
1963 September 23 - -
Korolev letter sets out a space exploration plan for 1965 to 1975. Nation: USSR. Spacecraft: Soyuz A, Soyuz B, Soyuz V, L2-1963, L3-1963, L4-1963, L5-1963. The plan included a series of lunar exploration vehicles: the L1, L2, L3, L4, and L5.
1963 September 23 - -
First child born to someone who has been in space. Nation: USSR. A daughter is born to Titov. This is the first child born to someone who has been in space. References: 376.
1963 September 23 - Launch Site: Fort Wingate. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 2044. -
Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Successful missile test. Missed aimpoint by 63 m. References: 2.
1963 September 23 - Launch Site: Vandenberg. Launch Complex: 395-D. Launch Pad: -. Launch Vehicle: Titan. Model< |