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Vanguard 3
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Class: Earth. Type: Magnetosphere. Nation: USA. Agency: U.S. Navy. Radiation, micrometeoroid data. Typical orbit: 512 km x 3413 km at 33 degrees inclination. Associated Launch Vehicle: Vanguard. Vanguard 3 Chronology - 1959 April 14 - Vanguard 3A - Program: Vanguard. Launch Site: Cape Canaveral. Launch Vehicle: Vanguard. FAILURE: Stage 2 damaged at seperation. Mass: 10 kg (22 lb). Apogee: 100 km (60 mi).
- 1959 June 22 - Vanguard 3B - Program: Vanguard. Launch Site: Cape Canaveral. Launch Vehicle: Vanguard. FAILURE: Stage 2 propulsion malfunction. Mass: 10 kg (22 lb). Apogee: 140 km (80 mi).
Bibliography and Further Reading
- McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
- Bramscher, Robert G, Spaceflight, "A Survey of Launch Vehicle Failures", 1980, Volume 22, page 351.
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