Vanguard 3
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).

  • 1959 September 18 - Vanguard 3 - Program: Vanguard. Launch Site: Cape Canaveral. Launch Vehicle: Vanguard. Mass: 23 kg (50 lb). Perigee: 512 km (318 mi). Apogee: 3,413 km (2,120 mi). Inclination: 33.40 deg. Period: 126.40 min.

    Radiation, micrometeoroid data. Third stage failed to separate from payload. The TV-4BU burned-out third stage was left attached to the payload since the fiberglas case did not adversely affect the experiments.


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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