Solid propellant rocket stage. Loaded mass 300 kg. Thrust 58.70 kN.
Status: Retired 1988.
Gross mass: 300 kg (660 lb).
Height: 3.70 m (12.10 ft).
Diameter: 0.23 m (0.75 ft).
Thrust: 58.70 kN (13,196 lbf).
Number: 123 .
More... - Chronology...
Associated Countries
Associated Engines
Associated Launch Vehicles
-
HJ Nike Hydac American sounding rocket. Three stage vehicle consisting of 1 x M-6 + 1 x Nike + 1 x Hydac More...
-
Nike Hydac American sounding rocket. Two stage vehicle consisting of 1 x Nike + 1 x Hydac More...
-
Sergeant Hydac American sounding rocket. Two stage vehicle consisting of 1 x Sergeant + 1 x Hydac More...
-
HJ Hydac American sounding rocket. Two stage vehicle consisting of 1 x M-6 + 1 x Hydac More...
-
Talos Sergeant Hydac American sounding rocket. Three stage sounding rocket consisting of 1 x Talos booster + 1 x Sergeant + 1 x Hydac More...
Associated Manufacturers and Agencies
-
Aerojet American manufacturer of rockets, spacecraft, and rocket engines. Aerojet, Sacramento, CA, USA. 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
