Encyclopedia Astronautica
DF-11-1


Solid rocket stage. 93.20 kN (20,952 lbf) thrust. Mass 5,400 kg (11,905 lb).

Status: M.
Gross mass: 5,400 kg (11,900 lb).
Unfuelled mass: 1,645 kg (3,626 lb).
Height: 7.40 m (24.20 ft).
Diameter: 0.88 m (2.88 ft).
Thrust: 93.20 kN (20,952 lbf).

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Associated Countries
Associated Engines
Associated Launch Vehicles
  • DF-11 Chinese single-stage solid-propellant short range ballistic missile. Export designation M-11, assembled as Ghaznavi in Pakistan. More...

Associated Manufacturers and Agencies
  • Sanjiang Chinese manufacturer of rocket engines and rockets. Sanjiang Space Group, Xiaogan, China. 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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