NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
New two-stage accelerator for hypervelocity impact simulationThe present knowledge of the micrometeoroid environment and the simulation requirements for laboratory devices show that the simulated mass-velocity range must be extended to higher values in both mass and velocity. This is accomplished with the new two-stage accelerator, which consists of a light gas gun as the first stage and a coaxial accelerator with a compressor coil as the second stage. The operation of the new device is described together with a theoretical investigation of the timing of the first and the second stage, which leads to an appropriate adjustment of the two stages. The theoretical and experimental results agree well and show that 600-micron diameter glass beads have been accelerated to velocities near 20 km/sec.
Document ID
19760031011
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Igenbergs, E. B.
(Muenchen, Technische Universitaet Munich, Germany)
Jex, D. W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Shriver, E. L.
(NASA Marshall Space Flight Center Space Sciences Laboratory, Huntsville, Ala., United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: AIAA Journal
Volume: 13
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
76A13977
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available