Solid rocket stage. 134.00 kN (30,124 lbf) thrust. Mass 2,600 kg (5,732 lb).
Status: Retired 1988.
Gross mass: 2,600 kg (5,700 lb).
Unfuelled mass: 350 kg (770 lb).
Height: 2.80 m (9.10 ft).
Diameter: 1.02 m (3.34 ft).
Thrust: 134.00 kN (30,124 lbf).
Burn time: 46 s.
Number: 58 .
More... - Chronology...
Associated Countries
Associated Engines
Associated Launch Vehicles
Associated Manufacturers and Agencies
-
Thiokol American manufacturer of rocket engines and rockets. Thiokol Corporation, Ogden, UT, USA. More...
-
Hercules American manufacturer of rocket engines and rockets. Hercules, Wilmington, Delaware, USA. More...
Associated Propellants
-
Solid Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. Solid propellants have the fuel and oxidiser embedded in a rubbery matrix. They were developed to a high degree of perfection in the United States in the 1950's and 1960's. In Russia, development was slower, due to a lack of technical leadership in the area and rail handling problems. More...
Home - Browse - Contact
© / Conditions for Use
