| astronautix.com | June 29 |
1955 - Nation: USA.
1956 - Nation: USA. Launch Site: White Sands . Launch Vehicle: Aerobee-Hi. LV Configuration: Aerobee-Hi.
Ionosphere research. Launched at 1200 local time. Reached 261 km.
1960 - - 22:00 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: LC75-3-4. Launch Vehicle: Thor Agena A. LV Configuration: Thor s/n 160 / Agena A s/n 1053. FAILURE: Failure.
KH-1 prototype; designed to test capsule recovery system; did not carry camera. References: 5 , 126 .
1961 - - 04:22 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17B. Launch Vehicle: Thor Able-Star. LV Configuration: Thor Ablestar s/n 315 AB008.
Carried SNAP-3A nuclear power source. References: 1 , 2 , 5 , 6 .
Dual launch; failed to separate from Solrad 3; still returned radiation data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 1 , 2 , 5 , 6 .
1962 - Nation: USA. Launch Vehicle: Minuteman 1A.
1962 - Nation: USA.
1962 - Nation: USA. Launch Site: Edwards . Launch Vehicle: X-15A. LV Configuration: X-15 No. 2 Flight 24.
Maximum Speed - 5278 kph. Maximum Altitude - 25360 m. References: 38 , 49 , 97 .
1963 - - 22:30 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: LC75-3-5. Launch Vehicle: TA Thor Agena B. LV Configuration: TA Thor s/n 380 / Agena B s/n 2314.
1964 - Nation: China. Launch Site: Jiuquan .
1965 - Nation: USA.
NASA launched Apollo mission PA-2, a test of the launch escape system (LES) simulating a pad abort at WSMR. All test objectives were met. The escape rocket lifted the spacecraft (boilerplate 23A) more than 1,524 m (5,000 ft) above the pad. The earth landing system functioned normally, lowering the vehicle back to earth. This flight was similar to the first pad abort test on November 7, 1963, except for the addition of canards to the LES (to orient the spacecraft blunt end forward after engine burnout) and a boost protective cover on the CM. PA-2 was the fifth of six scheduled flights to prove out the LES. References: 16 .
1965 - - 00:00 GMT. Nation: USA. Launch Site: Edwards . Launch Vehicle: X-15A. LV Configuration: X-15 No. 3 Flight 44.
Maximum Speed - 5522 kph. Maximum Altitude - 85527 m. Astronaut wings flight (USAF definition). References: 33 , 38 , 49 , 97 .
1966 - Nation: USA. Launch Site: Vandenberg . Launch Vehicle: Titan 3B.
Nation's initial launch of a satellite by a Titan IIIB/Agena space booster (first launch of a Titan III from Vandenberg AFB). References: 88 .
1967 - Nation: USA. Launch Site: Edwards . Launch Vehicle: X-15A. LV Configuration: X-15 No. 1 Flight 73.
Electrical failure while climbing through 32610 m; lost engine at 69 seconds; landed at Mud Lake with no flaps; Knight injured while exiting aircraft. Maximum Speed - 4618 kph. Maximum Altitude - 52730 m. References: 38 , 49 , 97 .
1967 - - 21:01 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: LE-6. Launch Vehicle: Thor Burner. LV Configuration: Thor Burner 2 s/n 171.
Location survey. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 1 , 2 , 5 , 6 .
Investigated aurora borealis. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). References: 1 , 2 , 5 , 6 .
1969 - Nation: UK. Launch Site: Woomera . Launch Vehicle: Black Arrow. LV Configuration: Black Arrow (2 stage). FAILURE: Control lost after 50 sec.
1969 - - 03:15 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17A. Launch Vehicle: Delta N. LV Configuration: Thor Delta N s/n 539 / Delta s/n 70.
Biological capsule reentered 7/7/69. The intent had been to fly a 6 kg male pig-tailed monkey (Macaca nemestrina) named Bonnie in Earth-orbit for 30 days. However, after only 8.8 days in orbit, the mission was terminated because of the subject's deteriorating health. High development costs were a strong incentive for maximising the scientific return from the mission. Because of this, the scientific goals had become exceedingly ambitious over time, and a great many measurements were conducted on the single research subject flown. Although the mission was highly successful from a technical standpoint, the science results were apparently compromised. Additional Details: Biosatellite 3. References: 1 , 2 , 5 , 6 , 297 .
1972 - - 03:47 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M / SOL.
Study of the processes of solar activity and of their influence on interplanetary space and the Earth's magnetosphere. References: 1 , 2 , 5 , 6 .
1974 - - 12:57 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Soyuz 11A511M.
Military topography satellite; returned film capsule; separated science capsule. References: 1 , 2 , 6 .
1974 - - 16:00 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC41/1. Launch Vehicle: Molniya 8K78M.
Covered Oko constellation plane 2 - 315 degree longitude of ascending node. References: 1 , 2 , 5 , 6 , 100 .
1976 - - 07:26 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Voskhod 11A57.
High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 1 , 2 , 6 .
1976 - - 09:21 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC132. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 53731-284.
1977 - - 18:43 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Vostok 8A92M.
Continuation of experimental work in studying the natural resources of the earth. Acquisition of meteorological information required for use in the operational weather service. References: 1 , 2 , 6 .
1978 - - 22:25 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC36B. Launch Vehicle: Atlas Centaur SLV-3D. LV Configuration: Atlas SLV-3D(R) s/n AC-41 / Centaur D-1AR s/n 5021.
US domestic telephone service. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit References: 1 , 2 , 5 , 6 , 278 .
1979 - - 16:04 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Soyuz 11A511U.
Photo surveillance; returned film capsule. References: 1 , 2 , 6 .
1980 - - 04:41 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n P15000-232.
Unmanned supply vessel for Salyut 6. Delivery of various cargoes to the Salyut-6 orbital station. Docked with Salyut 6 on 1 Jul 1980 05:53:00 GMT. Undocked on 17 Jul 1980 22:21:00 GMT. Destroyed in reentry on 19 Jul 1980 01:47:00 GMT. Total free-flight time 3.19 days. Total docked time 16.69 days. References: 1 , 2 , 6 , 275 .
1984 - - 00:28 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC90. Launch Vehicle: Tsyklon 2.
Ocean surveillance; nuclear powered. References: 1 , 2 , 5 , 6 .
1984 - - 14:52 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Soyuz 11A511U.
Military cartographic satellite; returned film capsule. References: 1 , 2 , 6 .
1991 - - 13:55 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC5. Launch Vehicle: Scout G. LV Configuration: Scout G-1 s/n S216C.
Radiation Experiment; tested communications components in high radiation environment. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 1 , 2 , 5 , 6 .