| astronautix.com | August 11 |
1950 - Nation: USA.
NACA flight 39. For pressure distribution and stability and control data. Check of stabilizer effectiveness. References: 49 , 97 .
1954 - Nation: USA. Launch Site: Holloman . Launch Vehicle: Aerobee. LV Configuration: RTV-A-1a.
Ionosphere research. Launched at 1025 local time. Reached 91.8 km.
1958 - - 09:30 GMT. Nation: USA. Launch Site: Johnson Island . Launch Complex: LC2. Launch Vehicle: Redstone. LV Configuration: Redstone s/n CC-51. FAILURE: Guidance system malfunction at 70 seconds which did not preclude subsequent system operations and successful mission accomplishment.
Orange was a rocket-launched test of the W-39 warhead. Purpose was to measure the effects of high altitude nuclear explosions in order to design warheads for Nike-Zeus anti-ballistic missile system. The Hardtack Configuration Redstone shot the 3.8 megaton warhead to an altitude of 43 km. References: 439 .
1959 - Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC13. Launch Vehicle: Atlas D. LV Configuration: Atlas 14D.
1961 - Nation: USA.
1962 - Nation: USA.
Of the 11 companies invited to bid on the lunar excursion module on July 25, eight planned to respond. NAA had notified MSC that it would not bid on the contract. No information had been received from the McDonnell Aircraft Corporation and it was questionable whether the Northrop Corporation would respond. References: 16 .
1962 - Nation: USA.
A NASA program schedule for the Apollo spacecraft command and service modules through calendar year 1965 was established for financial planning purposes and distributed to the NASA Office of Manned Space Flight, Marshall Space Flight Center, and MSC. The key dates were: complete service module drawing release, May 1, 1963; complete command module drawing release, June 15, 1963; manufacture complete on the first spacecraft, February 1, 1964; first manned orbital flight, May 15, 1965. This tentative schedule depended on budget appropriations. References: 16 .
1962 - - 08:30 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Vostok 8K72K.
Joint flight with Vostok 4. The first such flight, where Vostok capsules were launched one day apart, coming within a few kilometers of each other at the orbital insertion of the second spacecraft. The flight was supposed to occur in March, but following various delays, one of the two Vostok pads was damaged in the explosion of the booster of the third Zenit-2 reconnsat in May. Repairs were not completed until August. Vostok 3 studied man's ability to function under conditions of weightlessness; conducted scientific observations; furthered improvement of space ship systems, communications, guidance and landing. Immediately at orbital insertion of Vostok 4, the spacecraft were less than 5 km apart. Popovich made radio contact with Cosmonaut Nikolayev. Nikolayev reported shortly thereafter that he had sighted Vostok 4. Since the Vostok had no maneuvering capability, they could not rendezvous or dock, and quickly drifted apart. The launches did allow Korolev to offer something new and different, and gave the launch and ground control crews practice in launching and handling more than one manned spacecraft at a time. The cosmonaut took colour motion pictures of the earth and the cabin interior. Recovered August 15, 1962 6:52 GMT. Landed 48:02N 75:45 E. References: 1 , 2 , 5 , 6 , 16 , 32 , 33 , 60 , 175 .
1965 - - 14:31 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC36B. Launch Vehicle: Atlas Centaur LV-3C. LV Configuration: Atlas LV-3C s/n AC-6 / Centaur D s/n 151D.
Surveyor model launched dummy Surveyor payload into a barycentric / translunar orbit. References: 1 , 2 , 5 , 6 , 278 .
1966 - Nation: USA. Launch Site: Edwards . Launch Vehicle: X-15A. LV Configuration: X-15 No. 1 Flight 66.
Maximum Speed - 5776 kph. Maximum Altitude - 76500 m. References: 38 , 49 , 97 .
1970 - Nation: USA.
Maximum Speed - 1047 kph. Maximum Altitude - 19477 m. Flight Time - 413 sec. References: 49 , 97 .
1972 - Nation: USSR.
The Soyuz 7K-S had two parallel designs - the base variant, which was for special-purpose military solo missions; and a space station transport variant 7K-ST. The Soyuz 7K-S program was to consist of four unmanned, followed by two manned test flights, then two operational launches.
1972 - Nation: USA.
Maximum Speed - 1168 kph. Maximum Altitude - 20480 m. Flight Time - 375 sec. References: 49 , 97 .
1978 - Nation: USA.
1978 - Nation: USA.
1978 - Nation: USA.
1979 - Nation: USA.
Ferry flight, shuttle carrier aircraft/Enterprise (OV-101), Atlanta to St. Louis (1 hour, 50 minutes) References: 15 .
1979 - - 09:21 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U.
High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 1 , 2 , 6 .
1990 - - 20:24 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M / ML.
Operation of the long-range telephone and telegraph radio communications system in the USSR; transmission of USSR Central Television programmes to stations in the Orbita network and within the framework of international cooperation. References: 1 , 2 , 5 , 6 .
1993 - - 22:19 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n N15000-634.
Unmanned resupply vessel to Mir. Docked with Mir at the Kvant rear port on 13 Aug 1993 00:00:06 GMT. Undocked on 13 Oct 1993 17:59:06 GMT. Destroyed in reentry on 19 Oct 1993 00:22:14 GMT. Total free-flight time 7.33 days. Total docked time 61.75 days. References: 1 , 2 , 6 , 275 .
1994 - - 15:27 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC81L. Launch Vehicle: Proton 8K82K / 11S861. LV Configuration: Proton 8K82K s/n 367-02 / 11S861 s/n 74L.
Glonass navigation satellite. References: 2 , 5 , 6 , 67 , 274 .
Glonass navigation satellite. References: 2 , 5 , 6 , 67 , 274 .
Glonass navigation satellite. References: 2 , 5 , 6 , 67 , 274 .