Encyclopedia Astronautica
Jaguar 1-2


Solid propellant rocket stage. Loaded mass 200 kg. Thrust 140.00 kN.

Status: Retired 1964.
Gross mass: 200 kg (440 lb).
Height: 3.50 m (11.40 ft).
Diameter: 0.26 m (0.85 ft).
Thrust: 140.00 kN (31,470 lbf).
Burn time: 3.00 s.
Number: 10 .

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Associated Countries
Associated Engines
Associated Launch Vehicles
  • Jaguar 1 Three stage version consisting of 1 x Rook II + 1 x Gosling IIN + 1 x Lobster I More...

Associated Manufacturers and Agencies
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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