Encyclopedia Astronautica
Pershing 2-2


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 .

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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...

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