Comparison of theoretical and experimental steady wing loads on a space shuttle configuration at Mach numbers of 0.6 and 1.4 (NASA technical memorandum, NASA TM X-3404)

عربي : Български : 中文 : Česky : Deutsch : Dansk : Español : Suomi : Français : English : ελληνικά : Hrvatski : हिन्दी : Italiano : 日本語 : 한국어 : Nederlands : Norsk : Polski : Português : Română : Русский : Svenska

Classified Ads

Home | My Graand | Help


Comparison of theoretical and experimental steady wing loads on a space shuttle configuration at Mach numbers of 0.6 and 1.4 (NASA technical memorandum , NASA TM X-3404) (ID: B0006WPNUY)	Description and Photos \| More ads in Manuals & Literature

All Categories > Cars > Manuals & Literature

Classified Info:

Ad Format	Sell
Date of placing	2008-10-11 To expiration: 4 days
Availability	Whole World
www

Description and Photos

Comparison of theoretical and experimental steady wing loads on a space shuttle configuration at Mach numbers of 0.6 and 1.4 (NASA technical memorandum , NASA TM X-3404)

Recommend this ad to a friend | Get this links

© Copyright 2007 Interko Ltd. All Rights Reserved.
Designated trademarks and brands are the property of their respective owners.
Use of this Web site constitutes acceptance of the Graand User Agreement and Privacy Policy.