Star 37

Manufacturer Name: TE-M-364-1. Designer: Thiokol. Gross Mass: 621 kg (1,369 lb). Empty Mass: 63 kg (138 lb). Propellants: Solid. Thrust(vac): 43.500 kN (9,779 lbf). Thrust(sl): 33.600 kN (7,554 lbf). Isp: 260 sec. Isp (sea level): 220 sec. Burn time: 42 sec. Diameter: 0.66 m (2.16 ft). Length: 0.84 m (2.75 ft). Chambers: 1. Country: USA. First Flight: 1963. Last Flight: 1989. Flown: 180.

Total impulse 161,512 kgf-sec. Motor propellant mass fraction 0.899.

Star 37 used on Rocket Stages

Used on stage: Burner 2. on launch vehicle: Atlas LV-3A / Agena D.

Used on stage: Burner 2. on launch vehicle: Delta 0100.

Used on stage: Burner 2. on launch vehicle: Delta 1000.

Used on stage: Burner 2. on launch vehicle: Delta 2000.

Used on stage: Burner 2. on launch vehicle: Delta 3000.

Used on stage: Burner 2. on launch vehicle: Delta J.

Used on stage: Burner 2. on launch vehicle: Delta M.

Used on stage: Burner 2. on launch vehicle: N-2.

Used on stage: Burner 2. on launch vehicle: Thor Burner.

Used on stage: Burner 2. on launch vehicle: Thor Burner.

Used on stage: Burner 2. on launch vehicle: Titan 3BAS2.

Star 37 used on Spacecraft

Used on: GPS Block 2R.

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