200 inch solid, segment x 4

Propellants: Solid. Thrust(vac): 11,120.000 kN (2,499,870 lbf). Isp: 285 sec. Burn time: 175 sec. Diameter: 5.20 m (17.00 ft). Length: 35.10 m (115.10 ft). Chambers: 1. Country: USA. Status: Study 1960.

4 used as first stage of solid Nova design. Extended high-expansion nozzles. Specific impulse based on UA1205 solid motors of same period. Masses estimated based on total vehicle thrust, performance, and stage volumes.

200 inch solid, segment x 4 used on Rocket Stages

Used on stage: Nova Solid 4. on launch vehicle: Nova 5S.

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