burnout velocity


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burnout velocity

[′bərn‚au̇t və′läs·əd·ē]
(aerospace engineering)
The velocity of a rocket at the time when depletion of the fuel or oxidant occurs. Also known as all-burnt velocity; burnt velocity.
McGraw-Hill Dictionary of Scientific & Technical Terms, 6E, Copyright © 2003 by The McGraw-Hill Companies, Inc.

burnout velocity

The maximum velocity achieved by a rocket or missile at the termination of burning of propellant. The rocket or missile starts decelerating from this point.
An Illustrated Dictionary of Aviation Copyright © 2005 by The McGraw-Hill Companies, Inc. All rights reserved
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References in periodicals archive ?
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The role of airpower in active missile defense

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