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
Author information
JOURNAL FREE ACCESS

1986 Volume 2 Issue 1 Pages 2_16-2_27

Details
Abstract
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.
Content from these authors
© 1986 Japanese Rocket Society
Previous article Next article
feedback
Top