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NASA NTRS · 20020023126

Subsonic Glideback Rocket Demonstrator Flight Testing

Abstract

For the past two years, Cal Poly's rocket program has been aggressively exploring the concept of remotely controlled, fixed wing, flyable rocket boosters. This program, embodied by a group of student engineers known as Cal Poly Space Systems, has successfully demonstrated the idea of a rocket design that incorporates a vertical launch pattern followed by a horizontal return flight and landing. Though the design is meant for supersonic flight, CPSS demonstrators are deployed at a subsonic speed. Many steps have been taken by the club that allowed the evolution of the StarBooster prototype to reach its current size: a ten-foot tall, one-foot diameter, composite material rocket. Progress is currently being made that involves multiple boosters along with a second stage, third rocket.

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BibTeXRIS

DeTurris, Dianne J., Foster, Trevor J., Barthel, Paul E., Macy, Daniel J., Droney, Christopher K., Talay, Theodore A.. 2001-10-01. Subsonic Glideback Rocket Demonstrator Flight Testing. https://ntrs.nasa.gov/citations/20020023126

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