Encyclopedia Astronautica
JCR-1

Solid propellant rocket stage. Loaded mass 700 kg.

Status: Retired 1974.
Gross mass: 700 kg (1,540 lb).
Height: 7.00 m (22.90 ft).
Diameter: 0.50 m (1.64 ft).
Number: 10 .

Associated Countries

Associated Engines

Associated Launch Vehicles

Associated Manufacturers and Agencies

Nissan Japanese manufacturer of rocket engines and rockets. Nissan, Japan. 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...