February 29

See also Born on this Day
On this day in:

1944 - Launch Site: Peenemuende. Launch Vehicle: Wasserfall. LV Configuration: Wasserfall 2. FAILURE: Failure.

  • Wasserfall Test mission Nation: Germany. Agency: Wehrmacht.

1960 - Launch Vehicle: Saturn I.
  • Eleven companies submitted contract proposals for the Saturn second stage Nation: USA. Program: Apollo.

    Eleven companies submitted contract proposals for the Saturn second stage (S-IV): Bell Aircraft Corporation; The Boeing Airplane Company; Chrysler Corporation; General Dynamics Corporation, Convair Astronautics Division; Douglas Aircraft Company, Inc.; Grumman Aircraft Engineering Corporation; Lockheed Aircraft Corporation; The Martin Company; McDonnell Aircraft Corporation; North American Aviation, Inc.; and United Aircraft Corporation.

1960 - Launch Site: Cape Canaveral. Launch Complex: LC18. Launch Pad: LC18B. Launch Vehicle: Thor DM-18. Model: Thor DM-18C. LV Configuration: Thor DM-18C 263.
  • Thor DM-18 Special Test mission Nation: USA. Agency: USAF. Apogee: 520 km (320 mi).

1964 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 581.
  • Minuteman 1 Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1964 - Launch Site: Vandenberg. Launch Complex: LF05. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 636.
  • Minuteman 1 Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1964 - 05:32 GMT - Launch Site: Fort Churchill. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.44GE.
  • Nike Apache Auroral mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1968 - Launch Vehicle: Proton 8K82K / 11S824.
  • L1 commsision meeting. Nation: USSR. Program: Lunar L1. Spacecraft: Soyuz 7K-L1.

    For this L1 launch Chelomei wants to film separation of the first and second stages of the Proton rocket at 126 seconds into the flight - altitude 41 km, distance downrange 47 km. To do this two An-12 and one Tu-124 with long focal-length cameras will orbit 35 to 40 km from base. The discussion turns to how to recover the L1 if it lands in the ice-bound Aral Sea. The circle of possible landing points has a radius of 500 km from a point west of Karaganda. For political reasons it is not possible to deploy recovery forces to areas of Iran and India that are within this circle.

1968 - Launch Site: Baikonur. Launch Complex: PU31. Launch Vehicle: R-36. Model: R-36 8K67.
  • R-36 Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1968 - 17:15 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12. LV Configuration: MR-12 MR-12.
  • MR-12 Auroral mission Nation: USSR. Apogee: 170 km (100 mi).

1968 - 21:18 GMT - Launch Site: South Uist. Launch Vehicle: Petrel. LV Configuration: Petrel P6H.
  • Petrel Ionosphere mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi).

1976 - 01:15 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12. LV Configuration: MR-12 MR-12.
  • MR-12 Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 180 km (110 mi).

1976 - 03:30 GMT - Launch Site: Tanegashima. Launch Complex: N. Launch Pad: N. Launch Vehicle: N. Model: N-1. LV Configuration: N-1 N-2(F).
  • ISS 1 Nation: Japan. Payload: ISS a. Mass: 139 kg (306 lb). Class: Earth. Type: Ionosphere. Spacecraft: JISS. Agency: NASDA. Perigee: 988 km (613 mi). Apogee: 1,003 km (623 mi). Inclination: 69.70 deg. Period: 105.00 min. COSPAR: 1976-019A. USAF Sat Cat: 8709.

    Ionospheric sounding. Japanese Ionospheric Sounding Satellite (JISS - national name 'Ume') is intended for regular observations by means of radio waves of the global distribution of the critical frequencies of the ionosphere, and for utilization of the results of the observati on for radio wave forecasts and warning necessary for effective operation of short-wave radio-communication. Time of launch 0330UT.

1984 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Vehicle: Minuteman 2.
  • Minuteman 2 FOT GT146MS Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1988 - 08:34 GMT - Launch Site: Kiruna. Launch Vehicle: Black Brant. Model: Black Brant IX. LV Configuration: Black Brant IX MASER 2.
  • Black Brant Microgravity mission Nation: Sweden. Agency: SSC. Apogee: 318 km (197 mi).

1996 -
Born on this day in:
 
 
 
 
 
 
 
 
 

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 - 2007 except where otherwise noted.

 
Encyclopedia Astronautica
topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z