Cover image for Design of 450N nitrogen tetroxide and monomethyl hydrazine liquid propellant rocket engine for upper stage application
Title:
Design of 450N nitrogen tetroxide and monomethyl hydrazine liquid propellant rocket engine for upper stage application
Publication Information:
2009
Physical Description:
xxi, 99 p. : ill. ; 30 cm.
General Note:
Supervisor : Assoc. Prof. Dr. Subramaniam Krishnan

Also available in CD : CP 026991 ra
Subject Term:
Added Corporate Author:
DSP_DISSERTATION:
Project Paper (Sarjana Kejuruteraan (Mekanikal - Aeronautik)) - Universiti Teknologi Malaysia, 2009

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FKM30000005291 TL782 N66 2009 raf Closed Access Thesis UTM Project Paper (Closed Access)
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30000010227411 TL782 N66 2009 raf Closed Access Thesis UTM Project Paper (Closed Access)
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