Solid propellant rocket stage. Loaded mass 30 kg.
Status: Retired 1955.
Gross mass: 30 kg (66 lb).
Height: 1.00 m (3.20 ft).
Diameter: 0.13 m (0.42 ft).
Number: 16 .
More... - Chronology...
Associated Countries
Associated Engines
Associated Launch Vehicles
-
X-17 HTV American test vehicle. Three stage vehicle consisting of 1 x 3-DS-47000 + 3 x NOTS 124-C + 1 x NOTS 124-C More...
Associated Manufacturers and Agencies
-
NOTS American manufacturer of rocket engines and rockets. Naval Ordnance Test Station, China Lake, 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