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The acoustic cavity technique options and test validation of the bipropellant orbit control rocket engine(PDF)

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

Issue:
2006年05期
Page:
7-11
Research Field:
Publishing date:

Info

Title:
The acoustic cavity technique options and test validation of the bipropellant orbit control rocket engine
Author(s):
Hu Wei;  Li Ping
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
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PACS:
V431
DOI:
-
Abstract:
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References:

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Memo

Memo:
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Last Update: 1900-01-01