Encyclopedia Astronautica
MT-135JA-1


Solid propellant rocket stage. Thrust 12.00 kN.

Status: Active.
Height: 3.30 m (10.80 ft).
Diameter: 0.14 m (0.45 ft).
Thrust: 12.00 kN (2,697 lbf).
Number: 903 .

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Associated Countries
Associated Engines
Associated Launch Vehicles
  • MT-135 Japanese sounding rocket. The MT-135 was a small single-stage sounding rocket designed to collect data on the middle atmosphere, such as ozone layer depletion. More...
  • MT-135P Japanese sounding rocket. In 1969 the MT-135P was developed; featuring a parachute-equipped recoverable motor case for maritime safety. More...

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...

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