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Low supersonic stability and control characteristics of a 0.015-scale (remotely controlled elevon) model 44-0 space shuttle orbiter tested in the NASA/LARC 4 foot UPWT (LEG1) (LA101)

机译：在Nasa / LaRC 4英尺UpWT（LEG1）（La101）中测试的0.015比例（遥控升降舵）44-0型航天飞机轨道飞行器的低超音速稳定性和控制特性

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年度 1980
页码 1-366
总页数 366
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC STABILITY; CONTROLLABILITY; ELEVONS; SCALE MODELS; SPACE SHUTTLE ORBITERS; SUPERSONIC DRAG; WIND TUNNEL STABILITY TESTS; LATERAL CONTROL; SPACECRAFT MOTION; SPACECRAFT RELIABILITY; SUPERSONIC SPEED; WIND TUNNEL MODELS;

机译：空气动力学稳定性;可控性;升降副翼;尺度模型; spaCE sHUTTLE ORBITERs; sUpERsONIC DRaG;风洞稳定性试验;横向控制;航天器运动;航天器可靠性;超音速;风洞模型;

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Low supersonic stability and control characteristics of a 0.015-scale (remotely controlled elevon) model 44-0 space shuttle orbiter tested in the NASA/LARC 4 foot UPWT (LEG1) (LA101)

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