SR19
Target missile. Year: 1999. Family: Minuteman. Country: USA.

Single stage vehicle consisting of 1 surplus Minuteman 2 SR19AJ1 motor air-dropped from a C-130 transport. Similar to the SVC AltAir concept.

Manufacturer: Coleman. Launches: 2. Failures: 1. Success Rate: 50.00%. First Launch Date: 1997-01-30. Last Launch Date: 1999-03-31. Launch data is: continuing. Apogee: 100 km (60 mi). Liftoff Thrust: 267.000 kN (60,023 lbf). Total Mass: 8,000 kg (17,600 lb). Core Diameter: 1.32 m (4.33 ft). Total Length: 6.00 m (19.60 ft).



SR19 Chronology

1997 January 30 - Launch Site: Point Mugu. Launch Vehicle: SR19. FAILURE: The booster, while on a proper guidance trajectory, was destructed at 28 seconds due to a flight control anomaly.

  • AltAir (Have Gold) Test mission Nation: USA. Agency: USAF NAIC. Apogee: 15 km (9 mi). References: 1911.
1999 March 31 - 00:15 GMT - Launch Site: Barking Sands. Launch Pad: C-130. Launch Vehicle: SR19. LV Configuration: SR19 14.
  • SRALT/MBRV-3 Test mission Nation: USA. Agency: USA/USAF. Apogee: 100 km (60 mi). References: 1844.

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.
 
 
 
 
 
 
 
 
 

Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2007 except where otherwise noted.

 
Encyclopedia Astronautica
topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z