Encyclopedia Astronautica
Kappa 10S-2

Solid propellant rocket stage. Thrust 45.00 kN.

Status: Retired 1980.
Height: 2.00 m (6.50 ft).
Diameter: 0.42 m (1.37 ft).
Thrust: 45.00 kN (10,116 lbf).
Number: 19 .

Associated Countries

Associated Engines

Associated Launch Vehicles

Kappa 10S Japanese sounding rocket. Three stage vehicle consisting of 1 x K420H + 1 x K420(1/3) + 1 x K10S More...

Kappa 10 Japanese sounding rocket. 2-3 stage vehicle consisting of 1 x K420H + 1 x K420(1/3) More...

Kappa 10C Japanese sounding rocket. Two stage vehicle consisting of 1 x K420H + 1 x K420(1/3) 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...