首页> 美国政府科技报告 >SPACE SHUTTLE ORBIT MANEUVERING ENGINE REUSABLE THRUST CHAMBER TASKⅩ DATA DUMP COHPARISON OF 8- AND 10-INCH DIAMETER THRUST CHAMBERS
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SPACE SHUTTLE ORBIT MANEUVERING ENGINE REUSABLE THRUST CHAMBER TASKⅩ DATA DUMP COHPARISON OF 8- AND 10-INCH DIAMETER THRUST CHAMBERS

机译:空间穿梭轨道机动车发动机可重复使用推力室TasKⅩ数据转换8英寸和10英寸直径推力室

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Throe chamber configurations were analyzed: 1) an 8-inch diameter (Ec = 2) chamber having constant width channels;2) an 8-inch diameter chamber having constant width lands;and 3) a 10-inch diameter chamber (Ec = 3) having constant width lands. Component weights, pressure drops, and nozzle performance were calculated for each configuration using experimental heat transfer data. OMS trade factors were used to convert the weights and pressure drops to equivalent specific impulse values for: 1) constant OMS inert weight, and 2) constant OMS wet (tanked) weight.nThe resulting weights, pressure drops, and performance values summarized below indicate the superiority of the constant width land over the constant width channel configuration. The 8-inch diameter chamber provides a significant equivalent performance gain relative to the 10-inch chamber based on constant OMS inert weight but a slight perform-ance loss based on wet weight.

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  • 作者单位
  • 年度 1975
  • 页码 1-30
  • 总页数 30
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

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