Abstract: In this paper, the results of the LOX/propane propellant combustion test are presented,with the description of the thrust chamber test engine, the ignition, the combustion and the heat transfer. Also, the test results are compared with that of the N2O4/UDMH hynergolic propellant combustion test.

Key words: Combustion test;Propellant combustion;Hydrocarbon test;Engine test;Liquid propellant rocket engine

摘要： 本文介绍液氧/丙烷推进剂燃烧试验,包括试验件以及点火、燃烧、传热方面的试验情况;并与以往的四氧化二氮/偏二甲肼自燃推进剂的试验情况作了对比。

关键词: 燃烧试验;推进剂燃烧;烃类燃料;发动机试验;液体推进剂火箭发动机