Local Steady Aerodynamic Loads During Launch and Exit

NASA/SP-8006, Local Steady Aerodynamic Loads During Launch and Exit, NASA (Washington, DC, United States), May,1965, pp. 12, Format(s): PDF 1884k

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Local Steady Aerodynamic Loads During Launch and Exit, NASA SPACE VEHICLE DESIGN CRITERIA Volume 3: Structures. Part B: Loads and structural dynamics. Chapter 3: Launch and exit. Section 2: Local steady aerodynamic loads.

Keywords:	aerodynamic loads, differential pressure, dynamic structural analysis, spacecraft design, spacecraft launching, ventilation
CASI Document ID Number:	70N7160
Subjects:	Astronautics: Astronautics (General)
ID Code:	4
Deposited On:	10 May 2002