Encyclopedia Astronautica
ARPAT-2

Solid propellant rocket stage. Thrust 244.00 kN.

Status: Retired 1965.
Height: 3.10 m (10.10 ft).
Diameter: 0.71 m (2.32 ft).
Thrust: 244.00 kN (54,853 lbf).
Burn time: 11 s.

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...

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...