scholarly journals Problems of atmospheric wind inputs for missile and space vehicle design

1964 ◽  
Vol 1 (2) ◽  
pp. 181-184 ◽  
Author(s):  
JAMES R. SCOGGINS ◽  
WILLIAM W. VAUGHAN
Keyword(s):  
Space Vehicle ◽  
Vehicle Design

Human Factors in space vehicle design

2013 ◽  
Vol 92 (1) ◽  
pp. 110-118 ◽  
Author(s):  
Kritina L. Holden ◽  
Jennifer L. Boyer ◽  
Neta Ezer ◽  
Keith Holubec ◽  
Anikó Sándor ◽  
...  
Keyword(s):  
Human Factors ◽  
Space Vehicle ◽  
Vehicle Design

A reusable space vehicle design study exploring sharp leading edges

2001 ◽  
Author(s):  
James Reuther ◽  
David Kinney ◽  
Stephen Smith ◽  
Dean Kontinos ◽  
Peter Gage ◽  
...  
Keyword(s):  
Space Vehicle ◽  
Vehicle Design ◽  
Design Study ◽  
Leading Edges

Role of Applied Meteorology in the Development of Large Space Vehicles1

1963 ◽  
Vol 44 (3) ◽  
pp. 123-129 ◽  
Author(s):  
William W. Vaughan ◽  
James R. Scoggins ◽  
Orvel E. Smith
Keyword(s):  
Space Vehicle ◽  
Vehicle Design ◽  
Test Evaluation ◽  
Atmospheric Conditions ◽  
Large Space ◽  
General Outline ◽  
Vehicle Development ◽  
Applied Meteorology ◽  
Data Requirements

This paper discusses the role of applied meteorology in the solution of large space vehicle development problems. A general outline of the role of the applied meteorologist is given, followed by a discussion of the data requirements for vehicle design and test evaluation, analytical procedures for data presentation, and areas of influence on space vehicle development. Examples of the influence of atmospheric conditions in the design are presented illustrating the utility of applied meteorology.

scholarly journals Missions to Phobos and Other Minor Bodies

2002 ◽  
Vol 12 ◽  
pp. 642-645 ◽  
Author(s):  
Vsevolod S. Avduevsky ◽  
Efraim L. Akim ◽  
Timur M. Eneev ◽  
Mikhail Ya. Marov ◽  
Stanislav D. Kulikov ◽  
...  
Keyword(s):  
Space Vehicle ◽  
Space Mission ◽  
Vehicle Design ◽  
Sample Return ◽  
New Generation

AbstractA space mission to Mars’ moon Phobos with a space vehicle of new generation currently developed by the Russian Aerospace Agency is discussed. The vehicle design incorporates innovative SEP technology focused on small propulsion electric engines which significantly improve the mission energetic capability. The project is optimized around a sample return (PSR) from Phobos and also offers an opportunity for rendezvous/sample return missions from several asteroids, comets, and NEO. Scenario, rationale, and basic profile of PSR mission are presented.

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