See also Born on this Day On this day in: 1953 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Deacon. Model: Quad Deacon. -
Test launch Nation: USA. Agency: NACA. Apogee: 10 km (6 mi).
1957 -
1959 -
1960 - Launch Vehicle: Saturn V. -
Super booster program to be accelerated Nation: USA. Program: Apollo. President Dwight D. Eisenhower directed NASA Administrator T. Keith Glennan "to make a study, to be completed at the earliest date practicable, of the possible need for additional funds for the balance of FY 1960 and for FY 1961 to accelerate the super booster program for which your agency recently was given technical and management responsibility."
1960 - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 300. LV Configuration: Aerobee 300 TATTLETALE PCC 1. -
Signals intelligence test Nation: USA. Agency: USAF. Apogee: 100 km (60 mi).
1960 - 16:35 GMT - Launch Site: Cape Canaveral. Launch Complex: LC18B. Launch Pad: LC18B. Launch Vehicle: Delta. Model: Thor DM-18C. LV Configuration: Thor DM-18C 256. -
Special test Nation: USA. Agency: USAF. Apogee: 520 km (320 mi).
1961 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5. LV Configuration: R-5 V-1000 target. -
Target mission Nation: USSR. Agency: OKB-30. Apogee: 300 km (180 mi).
1961 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1E-14. FAILURE: Failure. -
Operational test Nation: USA. Agency: USN. Apogee: 20 km (12 mi).
1961 - 01:19 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7A.
1963 - -
Mercury spacecraft 15A was redesignated 15B and allocated as a backup for the MA-9 mission. Nation: USA. Program: Mercury. Spacecraft: Mercury. Flight: Mercury MA-10. In the event Mercury-Atlas 10 (MA-10) were flown, 15B would be the prime spacecraft. Modifications were started immediately with respect to the hand controller rigging procedures, pitch and yaw control valves, and other technical changes.
1964 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9a Sandia 152-21. -
Ballistic test Nation: USA. Agency: Sandia. Apogee: 292 km (181 mi).
1964 - 06:05 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 2. LV Configuration: Black Brant II AA-2-25. -
Auroral particles Aurora / ionosphere / micrometeorites mission Nation: Canada. Agency: NRCC. Apogee: 155 km (96 mi).
1965 - -
Apollo CM/SM umbilical cutter caused damage to the heatshield Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. During testing, it was found that blast effects of the linear charge for the CM/SM umbilical cutter caused considerable damage to the heatshield. To circumvent this problem, North American designed a vastly improved pyrotechnic-driven, guillotine-type cutter. MSC readily approved the new' device for both Block I and II spacecraft.
1965 - 12:00 GMT - Launch Site: Vandenberg. Launch Complex: 395-A3. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I SM-33. -
ST West Wind III operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,000 km (600 mi).
1966 - Launch Vehicle: N1. -
Korolev's death Nation: USSR. Program: Voskhod, Soyuz, Lunar L1. Spacecraft: Voskhod, Soyuz 7K-OK. Korolev dies at age 59 during what was expected to be routine colon surgery in Moscow. The day began for Kamanin with firm plans finally in place for the next three Voskhod and first three Soyuz flights. Volynov and Shonin will be the crew for the first Voskhod flight, with Beregovoi and Shatalov as their back-ups. That will be followed by a female flight of 15-20 days, with the crew begin Ponomaryova and Solovyova, with their back-ups Sergeychik (nee Yerkina) and Pitskhelaura (nee Kuznetsova). Tereshkova will command the female training group. Training is to be completed by March 15. After this Kamanin goes to his dacha, only to be called by General Kuznetsov around 19:00, informing him that Korolev has died during surgery. Kamanin does not minimise Korolev's key role in creating the Soviet space program, but believes the collectives can continue the program without him. In truth, Kamanin feels Korolev has made many errors of judgment in the last three years that have hurt the program. Mishin, Korolev's first deputy, will take over management of Korolev's projects. Kamanin feels that Mishin is a clever and cultured engineer, but he is no Korolev. Over the next three days the cosmonauts console Korolev's widow. Korolev's surgery was done personally by Petrovskiy, the Minister of Health. Korolev was told the surgery would take only a few minutes, but after five hours on the operating table, his body could no longer endure the insult, and he passed away.
1967 - 21:28 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 495 / Agena D SS-01B 1629.
1969 - 07:30 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511. -
Soyuz 4 Nation: USSR. Program: Soyuz. Payload: Soyuz 7K-OK (A) s/n 12. Mass: 6,625 kg (14,605 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-OK. Agency: MOM. Perigee: 213 km (132 mi). Apogee: 224 km (139 mi). Inclination: 51.70 deg. Period: 88.80 min. COSPAR: 1969-004A. USAF Sat Cat: 3654. Duration: 2.97 days. Decay Date: 1969-01-17. Crew: Shatalov. Flight: Soyuz 4, Soyuz 4/5. Soyuz 4 is launched with Vladimir Shatalov aboard without further problems at 10:30. This time the rockets gyroscopes, the capsule communications, and the television camera all functioned perfectly. Volynov and his crew for Soyuz 5 watched the launch from Area 17. Later Soyuz 4 would dock with Soyuz 5, and following a transfer of two cosmonauts, return with Shatalov, Yevgeni Khrunov and Alexsei Yeliseyev from Soyuz 5. Official purpose: scientific, technical and medico-biological research, checking and testing of onboard systems and design elements of space craft, docking of piloted space craft and construction of an experimental space station, transfer of cosmonauts from one craft to another in orbit. This mission finally successfully completed the simulated lunar orbit docking and crew transfer mission attempted by Soyuz 1 in April 1967. In making the transfer Khrunov and Yeliseyev avoided the most spectacular survivable incident of the space age - the nose-first reentry of Soyuz 5, still attached to its service module.
1969 - 10:00 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 10. LV Configuration: Kappa 10 K-10-4. -
Langmuir probe Infrared / x-ray astronomy / solar ultraviolet mission Nation: Japan. Agency: ISAS. Apogee: 229 km (142 mi).
1969 - 19:05 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Viper. Model: Viper-Dart. LV Configuration: Viper-Dart Sphere. -
Aeronomy mission Nation: USA. Agency: USA. Apogee: 147 km (91 mi).
1969 - 20:14 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy/Plasma mission Nation: USSR. Agency: AN SSSR. Apogee: 176 km (109 mi).
1970 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.453GM. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).
1970 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.452GM. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).
1970 - 01:10 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.343GM. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 160 km (90 mi).
1970 - 03:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.447CM. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 197 km (122 mi).
1970 - 04:06 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.64UE. -
Aurora mission Nation: USA. Agency: NASA. Apogee: 259 km (160 mi).
1970 - 04:41 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB AAF-VB-29. -
Auroral lower elevatuib Ionosphere / plasma / meteor mission Nation: Canada. Agency: NRCC. Apogee: 128 km (79 mi).
1970 - 05:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.448CM. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 204 km (126 mi).
1970 - 07:17 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.449CM. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 204 km (126 mi).
1970 - 09:15 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.450CM. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 201 km (124 mi).
1970 - 11:35 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.451CM. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 207 km (128 mi).
1970 - 18:43 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3B. LV Configuration: Titan 23B 23B-3 (3B-25).
1971 - -
VVS should support Almaz and Spiral. Nation: USSR. Program: Almaz, Salyut. Spacecraft: Salyut 1, Spiral OS. Kamanin discusses with Kutakhov the need for the VVS to back Chelomei rather than Mishin. As for the Spiral, the support of Dementiev, Afanasyev, Kalmykov, and Zverev have been lined up for the program. But Grechko is still blocking it. And Kutakhov is unwilling to challenge Grechko on the issue.
1971 - 12:00 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
1972 - -
Gilruth appointed NASA Director of Key Personnel Development Nation: USA. Program: Apollo. Manned Spacecraft Center Robert R. Gilruth was appointed to the newly created position of NASA Director of Key Personnel Development. He would integrate NASA planning to fill key positions, identify actual and potential candidates, and guide them through appropriate work experience. Christopher C. Kraft, Jr., MSC Deputy Director, was named Director of MSC. Both Kraft and Gilruth were original members of the NASA Space Task Group established in 1958 to manage Project Mercury.
1972 - 18:13 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P89T/C. -
ISRO 18.04 Ionosphere mission Nation: UK. Agency: SRC. Apogee: 128 km (79 mi).
1975 -
1975 - 20:56 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Ute Tomahawk. LV Configuration: Ute Tomahawk CRL A09.301-8. -
Aladdin 75 Reliability Test Aeronomy / test Nation: USA. Agency: USAF CRL. Apogee: 235 km (146 mi).
1977 - Launch Vehicle: Shuttle.
1977 - 10:18 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier Malemute. LV Configuration: Terrier Malemute NASA 29.03AE. -
Aurora / aeronomy / ionosphere mission Nation: USA. Agency: NASA. Apogee: 500 km (310 mi).
1980 - 19:49 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65067-248.
1981 - 22:00 GMT - Launch Site: Tanegashima. Launch Complex: T. Launch Pad: -. Launch Vehicle: S. Model: TT-500A. LV Configuration: TT-500A TT-500A-9F. -
Test mission Nation: Japan. Agency: NASDA. Apogee: 300 km (180 mi).
1982 - 07:51 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53767-250.
1983 - 20:40 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-76. -
Aeronomy / ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 349 km (216 mi).
1987 - 09:05 GMT - Launch Site: Plesetsk. Launch Complex: LC32. Launch Pad: LC32/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-3. -
Cosmos 1812 Nation: USSR. Program: Tselina. Payload: Tselina-D no. 59. Mass: 1,600 kg (3,500 lb). Class: Sigint. Spacecraft: Tselina-D. Agency: MO SSSR. Perigee: 598 km (371 mi). Apogee: 622 km (386 mi). Inclination: 82.50 deg. Period: 96.90 min. COSPAR: 1987-003A. USAF Sat Cat: 17295. Ocean surveillance.
1991 - 14:50 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 T15000-045.
1994 -
1996 - 11:10 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 7925. LV Configuration: Delta 7925 D231.
1998 - 21:12 GMT -
2002 - 08:23 GMT - Launch Site: Poker Flat. Launch Complex: LC4. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 12. LV Configuration: Black Brant XII NASA 40.14UE. -
SIERRA Ionosphere / aurora mission Nation: USA. Agency: NASA. Apogee: 735 km (456 mi).
2002 - 20:59 GMT - -
EVA ISS EO-4-1 Nation: USA. Program: ISS. Crew: Walz, Onufrienko. Flight: ISS EO-4. EVA Duration: 0.26 days. The spacewalk was made from the Pirs module. Depress was around 2050 UTC, with hatch open at 2059 UTC and egress around 2110 UTC. The astronauts moved the Strela-2 crane from PMA-1 to Pirs and installed it there; the Strela-1 crane was already functional on Pirs. They also installed an amateur radio antenna on Zvezda. On Jan 15 at about 0254 UTC the crew jettisoned two pairs of Orlan spacesuit gloves and a pair of towels used to wipe the spaceuits down, because of concerns about contamination from Zvezda thrusters. They reentered Pirs at 0255 UTC, with hatch close at 0302 UTC and repressurization above 50 mbar at about 0304 UTC.
2005 - -
Cassini, Titan Flyby Nation: USA. Spacecraft: Cassini.
2005 - -
Huygens Probe Lands on Titan, Successful Nation: USA. Spacecraft: Cassini.
Born on this day in:
- 1955 - Jeffrey Eliot Detroye. American Manned Spaceflight Engineer Astronaut. Birth City: Alexandria. Birth State: Virginia. Birth Country: USA.
- 1956 - William David Thompson. American Manned Spaceflight Engineer Astronaut. Birth City: Charleston. Birth State: West Virginia. Birth Country: USA.
Died on this day in: - 1966 - Sergei Pavlovich Korolev
. Russian Engineer.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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