Present information available on meteoroid environment of space and on hypervelocity impact and penetration is evaluated; guide line approach to development of design charts is established in terms of which attempt is made to assess effects on meteoroid shielding requirements of uncertainties in state-of-art information; if changing information requires extension of tables, necessary calculations can be made by means of equations given. (p 20-23, 55, 58, 60, 62, 64-66)
Meteoroid shielding for space vehicles
Aerospace Eng
Aerospace Engineering ; 19 , n 12
1960
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
NTIS | 2003
|NTRS | 2003
|Meteoroid Protection System for Space Vehicles
AIAA | 1963
|Advanced meteoroid and debris shielding concepts
AIAA | 1990
|