|
Engine Model: NOTS-3. Designer: NOTS. Gross Mass: 35 kg (77 lb). Empty Mass: 6.00 kg (13.20 lb). Propellants: Solid. Thrust(vac): 2.260 kN (508 lbf). Thrust(sl): 1.848 kN (416 lbf). Isp: 250 sec. Isp (sea level): 204 sec. Burn time: 25 sec. Chambers: 1. Country: USA. Status: Out of production. First Flight: 1960. Last Flight: 1962. Flown: 7.00.
NOTS-3 used on Rocket Stages
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 - 2008 except where otherwise noted.
|
|