Encyclopedia Astronautica
S-210-1


Solid propellant rocket stage. Loaded mass 200 kg.

AKA: S210.
Status: Retired 1982.
Gross mass: 200 kg (440 lb).
Height: 5.10 m (16.70 ft).
Diameter: 0.21 m (0.68 ft).
Number: 47 .

More... - Chronology...


Associated Countries
Associated Engines
Associated Launch Vehicles
  • S-210 Japanese sounding rocket. Single stage ionospheric sounding rocket used for research from Japan's Antarctic base. More...

Associated Manufacturers and Agencies
  • ISAS Japanese agency overseeing development of rockets, spacecraft, and rocket engines. Institute of Space and Astronautical Science, 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...

Home - Browse - Contact
© / Conditions for Use