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Class: Military. Type: Target. Destination: Medium Earth Orbit. Nation: USA. Agency: U.S. Air Force. Aluminum sphere used for radar calibration. Typical orbit: 1817 km circular orbit, 59.8 deg inclination.
LCS Chronology - 1965 May 6 - LCS 1 - Launch Site: Cape Canaveral. Launch Complex: LC20. Launch Vehicle: Titan. Mass: 34 kg (74 lb). Perigee: 2,786 km (1,731 mi). Apogee: 2,795 km (1,736 mi). Inclination: 32.10 deg. Period: 145.60 min.
Aluminum sphere used for radar calibration. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
- 1965 October 15 - LCS 2 - Launch Site: Cape Canaveral. Launch Complex: LC40. Launch Vehicle: Titan. FAILURE: Partial Failure. Perigee: 730 km (450 mi). Apogee: 785 km (487 mi). Inclination: 32.30 deg. Period: 99.98 min.
Dual launch with OV2-1; upper stage broke up.
- 1971 August 7 - LCS 4 - Launch Site: Vandenberg. Launch Complex: 576A2. Launch Vehicle: Atlas. Mass: 1.00 kg (2.20 lb). Perigee: 779 km (484 mi). Apogee: 910 km (560 mi). Inclination: 87.60 deg. Period: 101.80 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.
- Bramscher, Robert G, Spaceflight, "A Survey of Launch Vehicle Failures", 1980, Volume 22, page 351.
- Lockheed Martin Coporation, Atlas Family Fact Sheets, September 1998.. Web Address when accessed: http://www.lmco.com/ILS/txtmain/ils_lsysinfo.htm.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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