| astronautix.com | September 04 |
1927 - Nation: Russia.
1947 - Nation: USA.
AF flight 2. About mach 0.89. Telemeter failure required repeat of this flight. References: 49 , 97 .
1962 - Nation: USA.
Nine industry proposals for the lunar excursion module were received from The Boeing Company, Douglas Aircraft Company, General Dynamics Corporation, Grumman Aircraft Engineering Corporation, Ling-Temco-Vought, Inc., Lockheed Aircraft Corporation, Martin-Marietta Corporation, Northrop Corporation, and Republic Aviation Corporation. NASA evaluation began the next day. Additional Details: Nine industry proposals for the Apollo lunar excursion module received. References: 16 .
1965 - Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Molniya 8K78. LV Configuration: Molniya 8K78 s/n U103-27.
The launch was delayed due to malfunction of the RKS system of the Stages 1/2's control system during pre-launch service. References: 64 .
1968 - Nation: USA.
MSFC Director Wernher von Braun performed a full-pressure suit test in the Saturn I Workshop immersed in the Neutral Buoyancy Tank. He reported that the upgraded seals used in the aft dome penetration sealing study were 'very good,' but recommended additional handholds and tether points.
1979 - Nation: China. Launch Site: Wuzhai .
1981 - - 08:09 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U.
Photo surveillance; returned film capsule. References: 1 , 2 , 6 .
1981 - - 11:05 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC132. Launch Vehicle: Kosmos 11K65M.
Replaced Cosmos 926. Investigation of the upper atmosphere and outer space. References: 1 , 2 , 5 , 6 .
1982 - - 17:44 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC90. Launch Vehicle: Tsyklon 2.
Ocean monitoring. References: 1 , 2 , 5 , 6 .
1984 - - 10:33 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Soyuz 11A511U.
Military cartographic satellite; returned film capsule; maneuverable. References: 1 , 2 , 6 .
1984 - - 15:49 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC200P. Launch Vehicle: Proton 8K82K / 11S861. LV Configuration: Proton 8K82K s/n 320-01 / 11S861 s/n 5L.
Glonass. Testing components and apparatus from the space navigation system being set up to determine the position of Soviet civil aircraft and vessels in the Soviet merchant marine and fishing fleet. Three satellites launched by a single rocket. References: 1 , 2 , 5 , 6 , 67 , 274 .
Glonass. Testing components and apparatus from the space navigation system being set up to determine the position of Soviet civil aircraft and vessels in the Soviet merchant marine and fishing fleet. Three satellites launched by a single rocket. References: 1 , 2 , 5 , 6 , 67 , 274 .
Glonass. Testing components and apparatus from the space navigation system being set up to determine the position of Soviet civil aircraft and vessels in the Soviet merchant marine and fishing fleet. Three satellites launched by a single rocket. References: 1 , 2 , 5 , 6 , 67 , 274 .
1985 - - 07:12 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 65011-241.
Replaced Cosmos 1538. References: 1 , 2 , 5 , 6 .
1989 - - 04:19 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC40. Launch Vehicle: Titan 34D. LV Configuration: Titan 34D/Transtage s/n 34D-2 (05D-7).
Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
1996 - - 09:01 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC45L. Launch Vehicle: Zenit-2.
New heavy ELINT class. References: 4 .
1997 - - 12:03 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC36A. Launch Vehicle: Atlas IIAS. LV Configuration: Atlas IIAS (1N) s/n AC-146.
Geosynchronous. Stationed over 87.1W Launch vehicle put payload into supersynchronous earth orbit with IFR/MRS trajectory option. References: 4 , 278 .
Geosynchronous communications satellite. Stationed at 112 deg E.