Solid propellant rocket stage. Loaded mass 300 kg.
AKA: M-2.
Status: Retired 1965.
Gross mass: 300 kg (660 lb).
Height: 1.50 m (4.90 ft).
Diameter: 0.46 m (1.50 ft).
Number: 6 .
More... - Chronology...
Associated Countries
Associated Engines
Associated Launch Vehicles
-
Scout X-2M American all-solid orbital launch vehicle. Four stage vehicle consisting of 1 x Algol 1D + 1 x Castor + 1 x Antares 2 + 1 x MG-18 More...
-
Scout X-3M American all-solid orbital launch vehicle. Four stage vehicle consisting of 1 x Algol 2A + 1 x Castor + 1 x Antares 2 + 1 x MG-18 More...
-
Thor MG-18 American orbital launch vehicle. Two stage vehicle consisting of 1 x Thor DM-18A + 1 x MG-18 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...
Home - Browse - Contact
© / Conditions for Use