astronautix.com | Thor Able-Star |
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Thor Able Star - Credit: © Mark Wade. 992 bytes. 52 x 322 pixels. |
Launches: 20. Failures: 5. Success Rate: 75.00% pct. First Launch Date: 13 April 1960. Last Launch Date: 13 August 1965. LEO Payload: 150 kg. to: 620 km Orbit. Liftoff Thrust: 68,040 kgf. Total Mass: 53,000 kg. Core Diameter: 2.4 m. Total Length: 29.0 m. Flyaway Unit Cost $: 12.83 million. in 1985 unit dollars.
Navy TRANSIT I-B launched into orbit by Thor-Able-Star with navigation payload experiment at Cape Canaveral. Flight demonstrated the first engine restart in space and the feasibility of using satellites as navigational aids.
Solar radiation data. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).
Also returned geodetic data.
Experimental communications sattelite.
Experimental communications. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).
Destroyed by range safety; launched with Solrad 2. Thor shut down too early.
Dual launch; failed to separate from Transit 3B. Partial Failure.
Dual launch; failed to separate from Lofti 1. Partial Failure.
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).
Carried SNAP-3A nuclear power source.
Transit Research and Attitude Control. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).
Carried SNAP 3 nuclear power source.
![]() | Launch Complex 17B - Launch Complex 17B - Cape Canaveral 31,236 bytes. 238 x 371 pixels. |
Carried 5 satellites.
USN, USAF, US Army, NASA joint program.
Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).
The missions of Satellite 1963-038C were to measure omnidirectional flux of protons and electrons at various energy levels, radiation effects on transistors, and the effectiveness of thermal coatings. The satellite was launched together with a classified Department of Defense spacecraft on September 28, 1963. Its planned orbit was apogee 1120 kilometres, perigee 1070 kilometres, inclination 88.9 degrees. The satellite weighed 62 kg; its body was in the shape of an 0.46 m x 0.25 m octagonal prism. It was powered by four solar blades and transmited on 136, 162, and 324 mcs. The spacecraft was built for the Bureau of Naval Weapons. In 1967 it was still sending usable data from all systems.
Carried SNAP-9A nuclear power source.
Radiation monitoring.
Radiation monitoring.
Carried SNAP-9A nuclear power source.
Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
Celestial UV, magnetic field data.
Failed. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
Surveillance Calibration; dodecahedron; extended 12 25 ft. antennas. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
Surveillance Calibration; black 14 inch dia. sphere. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
Surveillance Calibration; white 14 inch dia. sphere.