See also Born on this Day On this day in: 1926 - Launch Vehicle: Goddard. Model: Goddard 1.
1953 - -
Gen. Dwight D. Eisenhower inaugurated president of United States Nation: USA.
1955 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5M. -
ZI test Nation: USSR. Agency: NII-88. Apogee: 500 km (310 mi).
1956 - Launch Site: Cape Canaveral. Launch Complex: LC3. Launch Pad: -. Launch Vehicle: X-17. LV Configuration: X-17 D-4. -
Test mission Nation: USA. Agency: USAF 6555ATW. Apogee: 132 km (82 mi).
1960 - Launch Vehicle: Soyuz. Model: R-7.
1960 - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1X-9. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1960 - 16:35 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7A. LV Configuration: R-7A I1-2.
1961 - -
Space Task Group management discusses a follow-on Mercury program. Nation: USA. Program: Gemini. Spacecraft: Gemini. Space Task Group management held a Capsule Review Board meeting. The first topic on the agenda was a follow-on Mercury program. Several types of missions were considered, including long-duration, rendezvous, artificial gravity, and flight tests of advanced equipment. Major conclusion was that a follow-on program needed to be specified in greater detail.
1961 - 20:53 GMT - Launch Site: Cape Canaveral. Launch Complex: LC19. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I AJ-10. FAILURE: Failure. -
Mk 4 re-entry vehicle test Nation: USA. Agency: USAF. Apogee: 0 km ( mi).
1964 - Launch Vehicle: Titan. Model: Titan 2. -
Martin-Baltimore conducted a static test-to-failure of the spacecraft/launch vehicle interface structure. Nation: USA. Test results demonstrated a very satisfactory minimum structural margin of 23 percent above ultimate conditions expected to be met in the transonic buffet conditions of launch. Plans were made to hold a structures meeting in Houston on March 17-19, 1964, for final review of all load conditions, stress distribution, and margins, in readiness for the Gemini-Titan 1 mission.
1964 - 17:02 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-57. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1964 - 18:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 2. LV Configuration: Black Brant II CC-2A-29. -
Fin test Nation: Canada. Agency: CARDE. Apogee: 204 km (126 mi).
1964 - 21:15 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 2. LV Configuration: Black Brant II CC-2A-30. -
Fin test Nation: Canada. Agency: CARDE. Apogee: 204 km (126 mi).
1965 - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. LV Configuration: Tomahawk Sandia 152-14. -
Magnus Stovepipe Test / aeronomy mission Nation: USA. Agency: Sandia. Apogee: 106 km (65 mi).
1965 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 777. -
Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).
1966 -
1966 - 15:17 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Little Joe II. Model: Little Joe II 5-2-2. LV Configuration: Little Joe II-5-2-2 LJII-5 (12-51-3). -
Apollo A-004 Nation: USA. Agency: NASA. Apogee: 23 km (14 mi).
1967 - Launch Vehicle: Saturn V. -
Apollo S-IVB stage for Saturn launch vehicle 503 exploded Nation: USA. Program: Apollo. The Saturn 503 S-IVB stage exploded and was destroyed at the Douglas Sacramento, Calif., Test Facility at 4:25 p.m. PST during a countdown. The exercise had progressed to 10 seconds before simulated launch (about 8 minutes before S-IVB ignition) when the explosion occurred.
- Additional details.
1969 - 04:14 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/D. LV Configuration: Proton-K/D 237-01. FAILURE: Second stage - One RD-0210 engine fails at T+510 sec, resulting in flight path deviation, automatic shutoff of launch vehicle. -
Soyuz 7K-L1 s/n 13L Nation: USSR. Program: Lunar L1. Payload: Soyuz 7K-L1 s/n 13L. Mass: 5,390 kg (11,880 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-L1. Agency: RVSN. COSPAR: F690120A. Decay Date: 1969-01-19. Launch failure - but the abort system again functioned perfectly, taking the capsule to a safe landing (in Mongolia!). At 501 seconds into the flight one of the four engines of the second stage shut down, and remained shut down for 25 seconds. The ever-reliable SAS abort system detected the failure, and separated the capsule from the failed booster. Yet again a successful capsule recovery after a booster failure.
- Additional details.
1970 - 20:20 GMT - Launch Site: Plesetsk. Launch Complex: LC133/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
1971 - -
Mishin pushing 'Big Orbital Station'. Nation: USSR. Program: Almaz, Salyut. Spacecraft: Almaz OPS, MKBS. Mishin is attempting to set up a separate training centre for civilian cosmonauts at the Moscow Aviation Institute. Mishin and the civilian cosmonauts come to view the TsPK premises to get ideas. This is a new attack by Mishin, in Kamanin's eyes. Mishin has been ill for a long time, but it doesn't stop him from meddling in the details of work of his deputies. Now they are working on a Big Orbital Station (BOS) for 9-12 crew. This amounts to nothing more than a new move against Chelomei. Mishin is intent on monopolising manned spaceflight at any cost. He attempts to take over any other such projects allocated to Chelomei or Kozlov.
1971 - 11:24 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
1971 - 23:45 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois SECEDE R13. -
PLUM Aeronomy mission Nation: USA. Agency: USAF. Apogee: 182 km (113 mi).
1972 - 18:36 GMT - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3D. LV Configuration: Titan IIID 23D-2.
-
OPS 7719 Nation: USA. Payload: SSF-B No. 22. Mass: 60 kg (132 lb). Class: Sigint. Spacecraft: SSF. Agency: NRO/USAF. Perigee: 474 km (294 mi). Apogee: 545 km (338 mi). Inclination: 96.00 deg. Period: 94.80 min. COSPAR: 1972-002D. USAF Sat Cat: 5772. Decay Date: 1979-04-17. Radar monitoring.
1973 - 03:36 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M Yu149-44.
1974 - Launch Site: Baikonur. Launch Complex: LC103. Launch Pad: -. Launch Vehicle: R-36M. -
POR state trials missile launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1975 - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5C. LV Configuration: Black Brant VC NASA 21.24US. -
LPSP-EUV4 Solar mission Nation: USA. Agency: NASA. Apogee: 279 km (173 mi).
1976 - Launch Site: WTR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3T. -
Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1976 - Launch Site: WTR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3T. -
Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1976 - 01:42 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 4B. LV Configuration: Black Brant IVB GL A16.501-01. -
VLF Ionosphere mission Nation: USA. Agency: USAF GL. Apogee: 632 km (392 mi).
1976 - 17:08 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53749-164.
1977 - 08:30 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1977 - 20:05 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53719-155.
1978 - 08:24 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. -
Progress 1 Nation: USSR. Program: Salyut 6. Payload: Progress s/n 102. Mass: 7,020 kg (15,470 lb). Class: Manned. Type: Logistics. Spacecraft: Progress. Agency: MOM. Perigee: 173 km (107 mi). Apogee: 256 km (159 mi). Inclination: 51.60 deg. Period: 88.70 min. COSPAR: 1978-008A. USAF Sat Cat: 10603. Duration: 18.73 days. Completed Operations Date: 1978-02-08 02:00:20 PM. Decay Date: 1978-02-08 02:00:20 PM. Flight: Salyut 6 EO-1. Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 22 Jan 1978 10:12:14 GMT. Undocked on 6 Feb 1978 05:54:00 GMT. Destroyed in reentry on 8 Feb 1978 02:00:00 GMT. Total free-flight time 3.91 days. Total docked time 14.82 days.
1981 - 04:50 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee F. LV Configuration: Astrobee F NASA 25.62DG. -
NRL far ultraviolet Spectrograph Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 209 km (129 mi).
1981 - 11:00 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1982 - 11:30 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1983 - 17:26 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M. -
Cosmos 1437 Nation: USSR. Program: Tselina. Payload: Tselina-D no. 39. Mass: 2,500 kg (5,500 lb). Class: Sigint. Spacecraft: Tselina-D. Agency: MOM. Perigee: 581 km (361 mi). Apogee: 604 km (375 mi). Inclination: 81.20 deg. Period: 96.50 min. COSPAR: 1983-003A. USAF Sat Cat: 13770.
1984 - 20:18 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Viper. Model: Viper 3A. LV Configuration: Viper 3A MAP/WINE. -
M-F 27 Aeronomy mission Nation: Germany. Agency: DFVLR. Apogee: 104 km (64 mi).
1986 - -
Rich Terrile's Discovery of Uranus Moons Cordelia & Ophelia Nation: USA.
1987 - 08:35 GMT - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. FAILURE: Failure. -
SENT-1 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 90 km (55 mi).
1988 - 22:51 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U2.
1990 -
1991 - 18:43 GMT - Launch Site: Scud Batteries. Launch Complex: -. Launch Pad: IRAQ-S. Launch Vehicle: R-17. Model: Al Hussein. -
Dhahran Nation: Iraq. Agency: IRAQ. Apogee: 100 km (60 mi).
1991 - 18:43 GMT - Launch Site: Scud Batteries. Launch Complex: -. Launch Pad: IRAQ-S. Launch Vehicle: R-17. Model: Al Hussein. -
Dhahran Nation: Iraq. Agency: IRAQ. Apogee: 100 km (60 mi).
1994 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-10. -
Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1994 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-10. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1994 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-10. -
Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1994 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-10. -
Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1994 - 09:49 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M 358-02.
1996 -
2005 - 03:00 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 411.
-
Universitetskiy Nation: Russia. Payload: Tatyana. Mass: 30 kg (66 lb). Class: Technology. Perigee: 911 km (566 mi). Apogee: 969 km (602 mi). Inclination: 83.00 deg. Period: 103.80 min. COSPAR: 2005-002C. USAF Sat Cat: 28523. Student satellite for radiation studies, ejected from Cosmos 2414. The satellite was built by students at MGU (Moskovskiy Gosudarstvenniy Universitet) for the university's 250th anniversary, and was nicknamed 'Tatyana' since the university's anniversary day is St. Tatyana's day
Born on this day in:
- 1948 - Jerry Lynn Ross. American Mission Specialist Astronaut. Birth City: Crown Point. Birth State: Indiana. Birth Country: USA.
Died on this day in: . American Engineer. Cause of Death: SSN 372-03-1426.
Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.
© Mark Wade, 1997 - 2008 except where otherwise noted.
|
|