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Subsonic Glideback Rocket Demonstrator Flight TestingFor 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.
Document ID
20020023126
Acquisition Source
Langley Research Center
Document Type
Other
Authors
DeTurris, Dianne J.
(California Polytechnic State Univ. San Luis Obispo, CA United States)
Foster, Trevor J.
(California Polytechnic State Univ. San Luis Obispo, CA United States)
Barthel, Paul E.
(California Polytechnic State Univ. San Luis Obispo, CA United States)
Macy, Daniel J.
(California Polytechnic State Univ. San Luis Obispo, CA United States)
Droney, Christopher K.
(California Polytechnic State Univ. San Luis Obispo, CA United States)
Talay, Theodore A.
Date Acquired
September 7, 2013
Publication Date
October 1, 2001
Subject Category
Spacecraft Design, Testing And Performance
Funding Number(s)
CONTRACT_GRANT: NAG1-2327
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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