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Class: Military. Type: Target. Nation: USA. Agency: U.S. Air Force. Space craft engaged in investigation of spaceflight techniques and technology. Typical orbit: 133 km x 1970 km at 92 degrees inclination. Mass: 364 kg (802 lb).
Cannonball Chronology - 1971 August 7 - Cannonball 2 - Launch Site: Vandenberg. Launch Complex: 576A2. Launch Vehicle: Atlas. Mass: 364 kg (802 lb). Perigee: 133 km (82 mi). Apogee: 1,970 km (1,220 mi). Inclination: 92.00 deg. Period: 106.30 min.
Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
Bibliography:- McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: http://www.planet4589.org/jsr.html.
- JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: http://msl.jpl.nasa.gov/home.html.
- Lockheed Martin Coporation, Atlas Family Fact Sheets, September 1998.. Web Address when accessed: http://www.lmco.com/ILS/txtmain/ils_lsysinfo.htm.
- McDowell, Jonathan, Launch Log, October 1998. Web Address when accessed: http://hea-www.harvard.edu/~jcm/space/log/launch.html.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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