Solid rocket stage. 9.80 kN (2,203 lbf) thrust. Mass 10 kg (22 lb).
Status: Retired 1954.
Gross mass: 10 kg (22 lb).
Unfuelled mass: 9.00 kg (19.80 lb).
Height: 1.20 m (3.90 ft).
Diameter: 0.0700 m (0.2290 ft).
Thrust: 9.80 kN (2,203 lbf).
Burn time: 0.90 s.
Number: 16 .
More... - Chronology...
Associated Countries
Associated Engines
-
Mk7 Multiple-source solid rocket engine. 9.8 kN. More...
Associated Launch Vehicles
-
FFAR American air-to-air rocket. Folding-Fin Air Rocket, boosted by 1 x Mk7. Unguided fighter weapon, later used as sounding rocket. More...
-
HVAR FFAR American test vehicle. Two stage vehicle consisting of 1 x HVAR + 1 x Mk7 More...
-
Double FFAR American test vehicle. Two stage vehicle consisting of 1 x Mk7 + 1 x Mk7 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
