|
RSA-3-1
|
|
Gross Mass: 10,215 kg (22,520 lb). Empty Mass: 1,100 kg (2,400 lb). Thrust (vac): 456.000 kN (102,512 lbf). Isp: 265 sec. Burn time: 52 sec. Propellants: Solid. Isp(sl): 240 sec. Diameter: 1.30 m (4.20 ft). Span: 2.30 m (7.50 ft). Length: 6.30 m (20.60 ft). Country: South Africa. No Engines: 1. Engine: RSA-3-1. Status: Out of production. First Flight: 1988. Last Flight: 1990. No Launched: 5. Used as: Shavit-1; NEXT-1; RSA-3 - 1. Source: Missile exhibit and placards, AF Museum, South Africa.
Used on Launch Vehicles:
|
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.
|
|
|
|