Design of 450N nitrogen tetroxide and monomethyl hydrazine liquid propellant rocket engine for upper stage application /

Project Paper (Sarjana Kejuruteraan (Mekanikal - Aeronautik)) - Universiti Teknologi Malaysia, 2009

Bibliographic Details
Main Authors: Noor Muhammad Feizal Muhalim, 1986-, Subramaniam Krishnan, supervisor, Fakulti Kejuruteraan Mekanikal
Format:
Published: 2009
Subjects: