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Some reentry experiments for investigating aerothermodybeen conducted to provide design guidelines for future reusable space transportation systems or hypersonic vehicles. Such studies evaluated the design aspects of aerothermodynamics The Sharp Edge Flight Experiment (SHEFEX) program is the main instance of such reentry missions. A launch vehicle for a reentry object is typically composed of two or more stages. propellant rocket VS-40 (Theil et al. Missions are programmed with sequenced events and they are guided based on nominal trajectories. In an uncontrolled Only between the penultimate stage burnout and the last maneuver) and spin-up maneuvers shall happen. The ignition vehicle into a descent one for the reentry. The pointing algorithm described here is based on the developed an algorithm to obtain a proper transfer from a

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