Solid rocket stage. 100.00 kN (22,481 lbf) thrust. Mass 1,500 kg (3,307 lb).
Status: Active.
Gross mass: 1,500 kg (3,300 lb).
Unfuelled mass: 100 kg (220 lb).
Height: 1.10 m (3.60 ft).
Diameter: 1.93 m (6.33 ft).
Thrust: 100.00 kN (22,480 lbf).
Burn time: 40 s.
Number: 22 .
More... - Chronology...
Associated Countries
Associated Engines
Associated Launch Vehicles
-
MSBS M4 French intermediate range ballistic missile. Submarine launched; MRV. Operational. 3 stage vehicle. More...
-
MSBS M45 French intermediate range ballistic missile. Improved M-4. 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...
Home - Browse - Contact
© / Conditions for Use
