| astronautix.com | March 30 |
1931 - Nation: Russia.
1943 - Nation: USA.
1948 - Nation: USA.
NACA flight 13. Stability and loads investigation. Mach 0.90. References: 49 , 97 .
1957 - Nation: Russia.
1959 - Nation: USA. Launch Vehicle: Jupiter.
Space Task Group personnel visited the Atlantic Missile Range at the invitation of the Army Ballistic Missile Agency to observe a Jupiter launch vehicle firing and the procedures followed on the day preceding the firing. The group toured the blockhouse and received briefings on various recorders that might be used in the centralized control facility for Mercury-Redstone and Mercury-Jupiter flights. References: 483 .
1961 - Nation: USA. Launch Site: Edwards . Launch Vehicle: X-15A. LV Configuration: X-15 No. 2 Flight 14.
Maximum Speed - 4441 kph. Maximum Altitude - 51700 m. References: 38 , 49 , 97 .
1961 - Nation: USA. Launch Vehicle: Saturn I RIFT.
Reactor-in-flight-test system (Rift) study, a part of the NASA-AEC program on nuclear rockets, was briefed by contractors at NASA headquarters. References: 18 .
1961 - - 20:34 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: LC75-3-4. Launch Vehicle: Thor Agena B. LV Configuration: Thor s/n 300 / Agena B s/n 1105. FAILURE: Second stage failed to obtain orbital velocity. Mechanical error.
KH-2; Mission failed. References: 5 , 126 .
1964 - Nation: USA. Launch Vehicle: Saturn V.
MSFC awarded Rocketdyne a definitive contract (valued at $158.4 million) for the production of 76 F-1 engines for the first stage of the Saturn V launch vehicle and for delivery of ground support equipment. References: 16 .
1965 - Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC18. Launch Vehicle: Blue Scout Junior. LV Configuration: Blue Scout Junior SLV-1B.
Suborbital. References: 5 .
1966 - Nation: USSR. Launch Vehicle: Soyuz 11A511U.
Ministry of General Machine Building (MOM) Decree 145ss 'On approval of the 7K-TK as transport for the Almaz station' was issued. It was decided that the 11F71 Soyuz-R space station would be cancelled and the Almaz would be developed in its place. Almaz was assigned the index number previously allocated to the Soyuz-R station, and Kozlov was ordered to hand over to Chelomei all of the work completed in relation to the station. However Kozlov's Soyuz 7K-TK ferry was to continue in development to transport crew to the Almaz. References: 474 .
1966 - Nation: USA. Launch Site: Vandenberg . Launch Vehicle: Thor.
Final mission of the Thor/Altair from Vandenberg AFB (first launch on 18 January 1965). References: 88 .
1966 - - 09:20 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: ABRESB3. Launch Vehicle: Atlas D. LV Configuration: Atlas D OV-1 (2x).
Optical radiation test. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 1 , 2 , 5 , 6 , 278 .
Thermal control experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 1 , 2 , 5 , 6 , 278 .
1967 - Nation: USSR.
Ministry of Defence Decree 'On formation of Anti-Space and Anti-Missile Forces of the Air Defence Forces (PKO) to operate General Soviet ASAT systems' was issued. References: 474 .
1967 - - 18:54 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC3W. Launch Vehicle: TA Thor Agena D. LV Configuration: Thor 2C s/n 501 / Agena D SS-01B s/n 1636.
KH-4A. Satellite flown nose first, all cameras operated satisfactorily. References: 1 , 2 , 5 , 6 .
1972 - - 14:09 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Vostok 8A92M.
Acquisition of meteorological information needed for use by the weather service. References: 1 , 2 , 5 , 6 .
1977 - - 23:02 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 53749-168.
Investigation of the upper atmosphere and outer space. References: 1 , 2 , 5 , 6 .
1978 - - 00:00 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC81P. Launch Vehicle: Proton 8K82K. LV Configuration: Proton 8K82K s/n 292-01.
Dual reentry test of two TKS-VA capsules. Recovered March 30, 1978 after one orbit. References: 1 , 2 , 5 , 6 , 67 , 274 , 439 .
Dual reentry test of two TKS-VA capsules. Recovered March 30, 1978 after one orbit. This test was four months behind the original schedule, due to the launch failure of August 4, 1978. References: 1 , 2 , 5 , 6 , 67 , 274 , 439 .
1978 - - 07:55 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U.
High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 1 , 2 , 6 .
1979 - Nation: USA.
Space shuttle main engine 2007, flight engine delivered to NSTL for acceptance test firing References: 15 .
1983 - - 01:12 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 65019-522.
Military navigation satellite. Replaced Cosmos 1344. References: 1 , 2 , 5 , 6 .
1986 - Nation: USSR. Launch Vehicle: Tu-2000.
In reaction to US X-30 project, Tupolev OKB asked to start work on counterpart. By 1992 mockup completed, but solving of propulsion and inlet problems intractable without access to supercomputers. References: 83 .
1987 - Nation: USSR. Launch Site: Baikonur . Launch Complex: Jubilee.
Time 25 minutes. References: 81 .
1988 - - 12:00 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U2.
Photo/digital surveillance. References: 1 , 2 , 6 .
1993 - - 03:09 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17A. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925 / Delta s/n 219.
Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
Small Expendable-tether Deployer System. References: 1 , 2 , 5 , 6 .
1993 - - 12:00 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC90. Launch Vehicle: Tsyklon 2.
First launch of new EORSAT, first of at 120 degree intervals on the same orbit with a 0 degree ascending node. Ocean surveillance. References: 1 , 2 , 5 , 6 , 69 .
1998 - - 06:02 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC2W. Launch Vehicle: Delta 7925. LV Configuration: Delta 7920-10C s/n 255.
Plane 3. Ascending node 230.9 degrees.
Plane 3. Ascending node 230.9 degrees.
Plane 3. Ascending node 230.9 degrees.
Plane 3. Ascending node 230.9 degrees.
Plane 3. Ascending node 230.9 degrees.