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A planetary ultra hypervelocity impact mechanics and shock wave science facilityUsing the concept of intercepting orbits from a pair of Space Station serviced free flyers, a class of impact and shock wave experiments pertinent to planetary science can be performed. One proposed free flying vehicle is an impactor dispensor, and the second is the impact laboratory. How collision is achieved by utilizing essentially twice orbital velocity is demonstrated. The impactor dispensor contains a series of small flyer plates or other projectiles which are launched into the trajectory of the impactor laboratory at appropriate positions. The impactor laboratory is a large impact tank similar to those in terrestrial gun laboratories, except that it contains a supply of targets and instrumentation such as high speed cameras, flash X-ray apparatus and digital recorders. Shock and isentropic pressures of up to 20 Mbar are achievable with such a system which provides 15 km/sec impact velocities for precisely oriented projectiles.
Document ID
19860017669
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ahrens, T. J.
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Publication Information
Publication: NASA. Lyndon B. Johnson Space Center Space Station Planetology Experiments (SSPEX)
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
86N27141
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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