Hyper-X Stage Separation: Background and StatusThis paper provides an overview of stage separation activities for NASA's Hyper-X program; a focused hypersonic technology effort designed to move hypersonic, airbreathing vehicle technology from the laboratory environment to the flight environment. This paper presents an account of the development of the current stage separation concept, highlights of wind tunnel experiments and computational fluid dynamics investigations being conducted to define the separation event, results from ground tests of separation hardware, schedule and status. Substantial work has been completed toward reducing the risk associated with stage separation.
Document ID
20040087154
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Reubush, David E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 99-4818Report Number: AIAA Paper 99-4818
Meeting Information
Meeting: 9th International Space Planes and Hypersonic Systems and Technologies Conference
Location: Norfolk, VA
Country: United States
Start Date: November 1, 1999
End Date: November 5, 1999
Sponsors: American Inst. of Aeronautics and Astronautics