Encyclopedia Astronautica
PAM-D2


Solid propellant rocket stage. Loaded/empty mass 3,697/431 kg. Thrust 107.20 kN. Vacuum specific impulse 282 seconds.

Cost $ : 5.890 million.

Status: Active.
Gross mass: 3,697 kg (8,150 lb).
Unfuelled mass: 431 kg (950 lb).
Height: 1.83 m (6.00 ft).
Diameter: 1.60 m (5.20 ft).
Span: 1.60 m (5.20 ft).
Thrust: 107.20 kN (24,099 lbf).
Specific impulse: 282 s.
Burn time: 120 s.
Number: 2 .

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Associated Countries
Associated Engines
  • Star 63 Thiokol solid rocket engine. 107.2 kN. Used in Shuttle,Titan 34D. Isp=282s. Used on Delta 7925 launch vehicle. First flight 1990. More...

Associated Launch Vehicles
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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