NDLI: Space shuttle orbiter reaction control system interactions with the vehicle flow field

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Space shuttle orbiter reaction control system interactions with the vehicle flow field

Content Provider	NASA Technical Reports Server (NTRS)
Author	Rausch, J. R.
Copyright Year	1978
Description	Test data on the effect of the interaction between the space shuttle orbiter rear-mounted reaction control system jets and the flow over the vehicle in the atmosphere are analyzed with particular attention to yaw angle effects. Masted tank-plus-orbiter jet interactions resulting from combinations of forward and rear-mounted reaction control jets being fired prior to external tank staging are also documented. The primary correlating parameter used for the mated data is a single-jet momentum ratioed to free-stream momentum. An analytic model for computing reaction control system interactions for all control combinations used for mated vehicle coast is included.
File Size	13644716
Page Count	394
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19780021199
Archival Resource Key	ark:/13960/t46q6rp0b
Language	English
Publisher Date	1978-05-01
Access Restriction	Open
Subject Keyword	Space Transportation Reaction Control Pitching Moments Jet Control Turbulent Wakes Flow Distribution Aerodynamic Interference Yawing Moments Thrust Control Orbital Maneuvers Space Shuttle Orbiters Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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