Encyclopedia Astronautica
RX-250-LPN-1


Solid propellant rocket stage. Loaded mass 300 kg. Thrust 52.00 kN.

Status: Active.
Gross mass: 300 kg (660 lb).
Height: 5.30 m (17.30 ft).
Diameter: 0.25 m (0.82 ft).
Thrust: 52.00 kN (11,690 lbf).
Burn time: 6.00 s.
Number: 5 .

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Associated Countries
Associated Engines
Associated Launch Vehicles
Associated Manufacturers and Agencies
  • LAPAN Indonesian manufacturer of rocket engines and rockets. Lembaga Penerbangan dan Antariksa Nasional (National Institute for Aeronautics and Space)Space), Indonesia. 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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