| 摘要 |
A space shuttle and a reentry attitude control of the space shuttle at low earth orbit are provided to secure stability of the space shuttle attitude reentering the low earth orbit without additional device. A space shuttle comprises a body(100), a nozzle(200) applying a propulsion force to the body, a rudder causing a yaw action in the body, a main wing(300) which is composed of a leading end(310) and a trailing end(320) with a first mounting groove(322) and attached to the body, an elevon which is mounted on the first mounting groove and moves to vary the attack angle, a tail boom(500) formed on the outer end of the main wing trailing end, and a canard(700) which is mounted apart from the main wing on the front side of the body and moves to vary the attack angle.
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