首页> 美国政府科技报告 >AERODYNAMIC RESULTS OF A SUPPORT SYSTEM INTERFERENCE EFFECTS TEST CONDUCTED AT NASA/LaRC UPWT USING AN 0.015-SCALE MODEL OF THE CONFIGURATION 140A/B SSV ORBITER (OA208)
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AERODYNAMIC RESULTS OF A SUPPORT SYSTEM INTERFERENCE EFFECTS TEST CONDUCTED AT NASA/LaRC UPWT USING AN 0.015-SCALE MODEL OF THE CONFIGURATION 140A/B SSV ORBITER (OA208)

机译:使用0.015比例的配置140a / B ssV轨道器(Oa208)在Nasa / LaRC UpWT上进行的支持系统干扰效果测试的空气动力学结果

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An experimental aerodynamic investigation (0A20B) was conducted in the NASA/LaRC UPWT from April 9 through April 12, 1974. The test article was the 0.015-scale 49-0 Mod. SSV Orbiter Configuration 140A/B model. The primary objective of this test was to determine the extent aerodynamic simulation of the Orbiter is affected by base mounting or the model, without MPS nozzles, on a straight sting.

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