Determination of launch-vehicle response to detailed wind profiles-Reference-Cited by-同舟云学术

Determination of launch-vehicle response to detailed wind profiles

Published:1965-01 Issue:1 Volume:2 Page:62-67
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

LESTER HAROLD C.¹,MORGAN HOMER G.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.28122

Reference20 articles.

1. APPROXIMATE TRANSFER FUNCTIONS FOR FLEXIBLE-BOOSTER-AND AUTOPILOT ANALYSIS

2. July 1959;Hobbs N. P.

3. Mazzola, L. L., Hobbs, N. P., and Criscione, E. S. "Wind, wind shear, and gust design criteria for vertically-rising vehicles as recommended on the basis of Montgomery, Alabama, wind data," Wright Air Development Div. TR 61-99 (1961); classified.

4. DESIGN CRITERIA FOR WIND-INDUCED FLIGHT LOADS ON LARGE BOOSTED VEHICLES

5. June 1963;Mazzola L. L.

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2. Elastic Launch Vehicle Response to Sinusoidal Gusts;Journal of Spacecraft and Rockets;1973-04

3. Nonstationary ascent wind analysis;14th Structures, Structural Dynamics, and Materials Conference;1973-03-20

4. Launch Vehicle Gust Penetration Loads;Journal of Spacecraft and Rockets;1972-01

5. Elastic launch vehicle response to sinusoidal gusts;12th Structures, Structural Dynamics and Materials Conference;1971-04-19