|Table of Contents|

Research on spontaneous combustion of C6H15N and HN03—27S(PDF)

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

Issue:
2008年06期
Page:
50-54
Research Field:
燃料与推进剂
Publishing date:

Info

Title:
Research on spontaneous combustion of C6H15N and HN03—27S
Author(s):
Niu XiaozheBian DongweiZhang Xiaojun
Xi,an Aerospace Propulsion Institute,Xi’an 7 1 0 l 00,China
Keywords:
C6H15NHN03—27Sspontaneous combustionmixture ratio
PACS:
V51l
DOI:
-
Abstract:
C6H15N and HN03—27S can be used as hypergolic propellant in I.ocket engines.The combustion capability was studied in this paper.The themodynamic characteristics were calculated by stepwise appmaching method.It was obtained that the optimal mixture mtio is 4.1 and the opti— mal sea level specific impulse is 2786Ⅱl/s at the combustion pressure of 4.5MPa.It is proVed by experiment that spontaneous coHlbustion of C6H15N and HN03—27S is feasible.

References:

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Last Update: 1900-01-01