The Journal of Space Technology and Science
Online ISSN : 2186-4772
Print ISSN : 0911-551X
ISSN-L : 0911-551X
Articles
M-3SII Motor Design
Masahiro KOHNO
著者情報
キーワード: M-3SII ROCKET, MOTOR DESIGN
ジャーナル フリー

1986 年 2 巻 1 号 p. 2_16-2_27

詳細
抄録
The M-3SII, the newest version of Mu launch vehicles, is a three stage, all solid propellant rocket motor enhanced by a strap-on booster system. It can carry 770 kg of payload to the low earth orbit (250 km circular) against the total mass of 62t. The paper will review the design and main characteristics of the M-3SII propulsion units.
著者関連情報
© 1986 Japanese Rocket Society
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