See also Born on this Day On this day in: 1943 - Launch Vehicle: JATO.
1943 - Launch Vehicle: V-2. -
Showdown meeting on A4 Nation: Germany. Speer meets with Von Braun and Dornberger. A 1:100 model of the planned bunker construction-launch facility for the rocket to be built by Organisation Todt on the British channel was exhibited. Speer reveals that Hitler could not decide about the rocket as a weapon. He did not believe the rocket team's plans could be made to work. But Speer did authorise them to proceed with construction on his own authority - he hoped Hitler could be brought around eventually. But he emphasised that Dornberger would have to use his personal connections to get industry moving on the project. But Dornberger was thwarted when the Army put Degenkolb in charge of organising production of the missile. Degenkolb was a sworn enemy of Dornberger's, and had been implicated in the 'suicide' of General Becker in early 1940. Degenkolb set up a Nazi-supported bureaucracy in parallel to that of Dornberger's, requiring the approval of the Army weapons bureau on any decisions. Degenkolb had the sponsorship of Todt and Saur, who in turn followed the party line - 'like the Fuehrer, we are not yet won over to the concept of a long range missile'. In order to productionise the A4 design, Degenkolb began authorising many detailed changes. He didn't understand that every change had to be proven in test first, and only incremental steps could be taken. Stahlknecht had planned to produce 300 A4 missiles per month by January 1944, and 600 per month by July 1944. Degenkolb unrealistically decreed that 300 per month be achieved by October 1943, and 900 per month by December 1943.
1947 -
1948 -
1957 - Launch Site: Cape Canaveral. Launch Complex: LC3. Launch Pad: -. Launch Vehicle: X-17. LV Configuration: X-17 R-18 4203-18. -
Re-entry vehicle test Nation: USA. Agency: USAF 6555ATW. Apogee: 140 km (80 mi).
1958 - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp II8.35. -
Test mission Nation: USA. Agency: USAF. Apogee: 145 km (90 mi).
1959 - Launch Vehicle: Redstone. Model: Redstone MRLV.
1960 - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1X-7. -
Inertial test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1964 - -
NASA criticises Manned Orbiting Laboratory. Nation: USA. Spacecraft: MORL. In an interview for Space Business Daily, Edward Z. Gray, Director of Advanced Studies in NASA's Office of Manned Space Flight, predicted that NASA's manned space station would be more sophisticated than the Defense Department's Manned Orbiting Laboratory. NASA had more than a dozen study projects under way, Gray said, that when completed would enable the agency to appraise requirements and pursue the best approach to developing such a space station.
1964 - 00:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-50. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1964 - 13:15 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.129IA. -
ISRO 10.02? (Na) Aeronomy mission Nation: USA. Agency: NASA. Apogee: 187 km (116 mi).
1964 - 20:10 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 1-43-69. FAILURE: Inertial instruments failure.
1965 - 18:59 GMT - Launch Site: Vandenberg. Launch Complex: OSTF2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 106F. -
ST Nation: USA. Agency: USAF SAC. Apogee: 1,400 km (800 mi).
1966 - -
Space trainers Nation: USSR. Program: Voskhod, Soyuz. Spacecraft: Voskhod, Soyuz 7K-OK. Flight: Voskhod 3, Voskhod 4, Voskhod 5, Soyuz 1, Soyuz 2A. Tyulin and Mozzhorin review space simulators at TsPK. The 3KV and Volga trainers are examined. Tyulin believes the simulators need to be finished much earlier, to be used not just to train cosmonauts, but as tools for the spacecraft engineers to work together with the cosmonauts in establishing the cabin arrangement. This was already done on the 3KV trainer, to establish the new, more rational Voskhod cockpit layout. Tyulin reveals that the female Voskhod flight now has the support of the Central Committee and Soviet Ministers. He also reveals that MOM has promised to accelerate things so that four Voskhod and five Soyuz flights will be conducted in 1966. For 1967, 14 manned flights are planned, followed by 21 in 1968, 14 in 1969, and 20 in 1970. This adds up to 80 spaceflights, each with a crew of 2 to 3 aboard. Tyulin also supports the Kamanin position on other issues - the Voskhod ECS should be tested at the VVS' IAKM or Voronin's factory, not the IMBP. The artificial gravity experiment should be removed from Voskhod and replaced by military experiments. He promises to take up these matters with Korolev.
1966 - 04:48 GMT - Launch Site: Vandenberg. Launch Complex: SLC10W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Burner 1. LV Configuration: Thor Burner 1 251. FAILURE: Second stage failed.
1966 - 13:11 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C103 TERLS-35. -
ISRO 15.03 Aeronomy / ionosphere mission Nation: India. Agency: ISRO. Apogee: 150 km (90 mi).
1968 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-273. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1969 -
1969 - -
Concern over the possibility of Soyuz 4 or 5 landing in the Aral Sea continues. Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 4, Soyuz 5, Soyuz 4/5. An Il-14 is sent on a flight to reconnoitre. It reports 12 to 50 cm ice over the entire surface. Mishin, Chertok, and the rest of he OKB-1 entourage arrive. An argument immediately ensures over provisions and planning for emergency landings. It is decided to make a review of emergency landing and recovery plans as the first agenda item every day of he flights.
1969 - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: S-250. LV Configuration: S-250 SO-250-B. -
Test mission Nation: Japan. Agency: ISAS. Apogee: 100 km (60 mi).
1969 - 02:10 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-25. -
Gyro-plasma probe Ionosphere / chemical release / fields mission Nation: Japan. Agency: ISAS. Apogee: 343 km (213 mi).
1970 - -
Dale D. Myers was appointed NASA Associate Administrator for Manned Space Flight. Nation: USA. Dale D. Myers was appointed NASA Associate Administrator for Manned Space Flight with an effective date of 12 January. He succeeded George E. Mueller, who left NASA on 10 December 1969 to become a vice president of General Dynamics Corporation. Prior to his acceptance of the NASA position, Myers was Vice President and General Manager of the Space Shuttle Program at North American Rockwell.
1971 - 21:41 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.016-3. -
Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 278 km (172 mi).
1971 - 22:11 GMT - Launch Site: Green River. Launch Complex: Pad 3. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena V144D. -
Re-entry Vehicle test Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).
1971 - 22:31 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.015-2. -
Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 276 km (171 mi).
1973 - 06:55 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/D. LV Configuration: Proton-K/D 259-01. -
Luna 21 Nation: USSR. Program: Luna. Payload: Ye-8 s/n 204. Mass: 5,567 kg (12,273 lb). Class: Planetary. Type: Lunar. Spacecraft: Luna Ye-8. Agency: MOM. Perigee: 90 km (55 mi). Apogee: 110 km (60 mi). Inclination: 60.00 deg. Period: 118.00 min. COSPAR: 1973-001A. USAF Sat Cat: 6333. Decay Date: 1973-01-15. The Proton / Block D launcher put the spacecraft into Earth parking orbit followed by translunar injection. On 12 January 1973, Luna 21 braked into a 90 x 100 km orbit about the Moon. On 13 and 14 January, the perilune was lowered to 16 km altitude. On 15 January after 40 orbits, the braking rocket was fired at 16 km altitude, and the craft went into free fall. At an altitude of 750 meters the main thrusters began firing, slowing the fall until a height of 22 meters was reached. At this point the main thrusters shut down and the secondary thrusters ignited, slowing the fall until the lander was 1.5 meters above the surface, where the engine was cut off. Landing occurred at 23:35 GMT in LeMonnier crater at 25.85 degrees N, 30.45 degrees E. The lander carried a bas relief of Lenin and the Soviet coat-of-arms. After landing, Lunokhod 2 took TV images of the surrounding area, then rolled down a ramp to the surface at 01:14 GMT on 16 January and took pictures of the Luna 21 lander and landing site. It stopped and charged batteries until 18 January, took more images of the lander and landing site, and then set out over the Moon. The rover would run during the lunar day, stopping occasionally to recharge its batteries via the solar panels. At night the rover would hibernate until the next sunrise, heated by the radioactive source. Lunokhod 2 operated for about 4 months, covered 37 km of terrain including hilly upland areas and rilles, and sent back 86 panoramic images and over 80,000 TV pictures. Many mechanical tests of the surface, laser ranging measurements, and other experiments were completed during this time. On June 4 it was announced that the program was completed, leading to speculation that the vehicle probably failed in mid-May or could not be revived after the lunar night of May-June. The Lunokhod was not left in a position such that the laser retroreflector could be used, indicating that the failure may have happened suddenly.
1974 - 01:40 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.22DG-DP. -
NRL NB12.271 Aeronomy / extreme ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 193 km (119 mi).
1976 - Launch Site: Vandenberg. Launch Complex: LF26. Launch Pad: LF26?. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-12. -
Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).
1977 - 19:03 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.1008UE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 138 km (85 mi).
1982 -
1984 - 20:00 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Viper. Model: Viper 3A. LV Configuration: Viper 3A MAP/WINE. -
M-F 16 Aeronomy mission Nation: Germany. Agency: DFVLR. Apogee: 118 km (73 mi).
1986 - 11:25 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1987 -
1990 - 20:23 GMT -
1991 - 00:53 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 7925. LV Configuration: Delta 7925 D202.
1994 - 10:05 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U2. -
Soyuz TM-18 Nation: Russia. Program: Mir. Payload: Soyuz TM 11F732 s/n 67. Mass: 7,150 kg (15,760 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz TM. Agency: MOM. Perigee: 244 km (151 mi). Apogee: 335 km (208 mi). Inclination: 51.60 deg. Period: 90.10 min. COSPAR: 1994-001A. USAF Sat Cat: 22957. Duration: 182.02 days. Decay Date: 1994-07-09. Crew: Afanasyev, Polyakov, Usachyov. Flight: Mir EO-15, Mir EO-14, Mir LD-4. Mir Expedition EO-15. Docked at the Kvant module on January 10 at 11:15 GMT. Transported to the Mir orbital station of a crew comprising the cosmonauts V M Afanasev, Y V Usachev, and V V Polyakov for the fifteenth main expedition.
1999 -
Born on this day in:
- 1922 - Dale Dehaven Myers. American Manager. Birth City: Kansas City. Birth State: Missouri. Birth Country: USA.
- 1951 - Taufik Akbar. Indonesian Payload Specialist Astronaut. Birth City: Medan. Birth Country: Indonesia.
Died on this day in: . American Manager. Cause of Death: Greenwich, Fairfield, CT, SSN 124-28-5042.
- 1994 - Kenneth P Timmons. American Engineer.
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