S-56
Class: Earth. Type: Atmosphere. Nation: USA. Agency: U.S. Air Force.

12 foot diameter. balloon; atmospheric density studies.

Typical orbit: 757 km x 2433 km at 39 degrees inclination. Mass: 6.50 kg (14.30 lb). Associated Launch Vehicle: Scout X-1.


S-56 Chronology
  • 1960 December 4 - Explorer (9) S 56 - Program: Explorer. Launch Site: Wallops Island. Launch Vehicle: Scout X-1. FAILURE: Second stage malfunction. Mass: 6.00 kg (13.20 lb).

  • 1961 February 16 - Explorer 9 - Program: Explorer. Launch Site: Wallops Island. Launch Vehicle: Scout X-1. Mass: 7.00 kg (15.40 lb). Perigee: 757 km (470 mi). Apogee: 2,433 km (1,511 mi). Inclination: 38.80 deg. Period: 118.00 min.

    12 foot dia. balloon; atmospheric density studies. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).


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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