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Scheme of Chinese manned lunar rocket and its propulsion system(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2009年02期
Page:
1-6
Research Field:
专论与综述
Publishing date:

Info

Title:
Scheme of Chinese manned lunar rocket and its propulsion system
Author(s):
Zhang Xiaoping; Ding Fengnian; Ma Jie
Xi'an Aerospace Propulsion Institute，Xi'an 710100，China
Keywords:
manned lunar excursion; liquid rocket engine; thrust; propellant; cycle system
PACS:
V434
DOI:
-
Abstract:
Research and using of the moon is one of the focuses on aerospace development in 21th century．The technical path of manned lunar heavy launch vehicle in China and its propulsion system is discussed．The concept of developing heavy LOX／hydrocarbon and LOX／IJ-]2 liquid rocket en舀．es is put forward．The propellant combinations of heavy LOX／hydrocarbon liquid rocket engine， the cycle systems and the thrust level are discussed．The LOX／hydrocarbon propellant combination is chosen for non-toxic low cost and higll performance．Advanced staged combustion cycle or low cost gas generator cycle should be chosen and the thrust should be about 4000kN．

References:

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Last Update: 1900-01-01