Meteoroid/Orbital Debris Risk Assessment for Resuseable Launch Vehicles Using Metallic TPS

Meteoroid/Orbital Debris Risk Assessment for Resuseable Launch Vehicles Using Metallic TPS

Author(s):

Publication title:

A collection of technical papers : 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference : 11th AIAA/ASME/AHS Adaptive Structures Forum : 4th AIAA Gossamer Spacecraft Forum : AIAA Dynamics Specialists Conference, Norfolk, Virginia, 7-10 April 2003

Title of ser.:

AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference

Ser. no.:

2003

Pub. Year:

2003

Vol.:

v. 2

No.:

2003-1553

Paper no.:

AIAA-2003-1553

Page(from):

1421

Page(to):

1429

Pages:

9

Pub. info.:

Reston, Va: American Institute of Aeronautics and Astronautics

ISBN:

9781563476259 [1563476258]

Language:

English

Call no.:

A07400/031401 (v.2)

Type:

Technical Paper

Details

TDL ID:	ZA00001565
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ; AIAA/ASME/AHS Adaptive Structures Forum ; AIAA Gossamer Spacecraft Forum ; AIAA Dynamics Specialists Conference
Conf. info. (Number):	44th ; 11th ; 4th
Conf. info. (Venue):	Norfolk, Virginia
Conf. info. (Date):	2003.04.07-2003.04.10

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