2016년 7월 29일 금요일

S-300 rocket

S-300 rocket

S-300 rocket is the observation rocket which old Tokyo University Institute of Space and Aeronautical Science (ISAS) (existing Japan Aerospace Exploration Agency Institute of Space and Astronautical Science) developed in an IX plan. In addition, I describe the PT-300 rocket which is the prototype of the rocket in this clause.

Table of contents

Summary

It is S-300 rocket to have been developed parallel to S-210 rocket for Antarctic observation use of National Institute of Polar Research. The PT-300 rocket which was prototype flew normally in (1966) in 1966 and arrived at an altitude of 160km. I received this success, and the S-300 rocket was produced, and three planes flew from the first unit to the third unit in (1969) in 1969, but abnormality occurred in a body burning to two planes of those. About the abnormal cause, it was supposed that it was convincing that an attack angle was abnormally enhanced by pace roll resonance. A policy to evade resonance by wearing a spin from all over the flight positively in large in gas is devised, and I change it, and S-310 rocket will be developed in people of contracting business by Nissan Motor, Nippon Oil & Fats.

Mitsubishi Heavy Industries, Daisel performed the production.

Specifications

PT-300
  • Full length: 6,487.5mm
  • A diameter: 300mm
  • Gross weight: 668.9 kg
  • Deployment weight: 32.2 kg
  • Arrival is high: 160km
S-300
  • Full length: 6.5m
  • A diameter: 300mm
  • Gross weight: 660 kg
  • Deployment weight: 55 kg (構造部含)
  • Arrival is high: 160km

Flight results

Number Flight date and time (JST) Place Arrival is high Experiment contents
PT-300-1 1966 November 4 11:05 KSC 160km Flight performance test
S-300-1 1969 January 9 KSC
S-300-2 August 24 KSC
S-300-3 September 8 KSC

Allied item

Outside link

This article is taken from the Japanese Wikipedia S-300 rocket

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