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>From on-line searches, I've found lifting bodies like the M2F3 [1] have less than stellar low speed handling. For the spacecraft designer with a healthy mass budget, pop-out wings (hidden during re-entry) seem like a reasonable solution. Two questions regarding this idea: 1) Does the M2F3 lifting body configuration have high drag at subsonic speeds? I know it went supersonic during testing, but that could be indicative of high thrust, not low drag. 2) If the pop-out wings were designed for best low-speed (landing) performance, and the lifting body had a landing mass of 15 tons, what would a reasonable wing mass be? 500kg? 1000kg? 3000kg? [1] http://www.astronautix.com/craft/m2f3.htm Mike Miller, Materials Engineer
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