Accession Number : ADA625015


Title :   DebrisLV Hypervelocity Impact Post-Shot Physical Results Summary


Descriptive Note : Final rept.


Corporate Author : AEROSPACE CORP EL SEGUNDO CA


Personal Author(s) : Sheaffer, Patti M ; Adams, Paul M ; Hemmi, Naoki ; Hartney, Christopher


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a625015.pdf


Report Date : 27 Feb 2015


Pagination or Media Count : 55


Abstract : The DebrisLV ( Launch Vehicle ) target was a value-added, companion target to the full-scale satellite target (i.e., DebriSat) in the joint NASA/SMC-funded DebriSat Hypervelocity Impact Experiment. DebrisLV was conceived and built at The Aerospace Corporation in the Remote Sensing Department of the Space Sciences Applications Laboratory, Laboratory Operations, Engineering and Technology Group. DebrisLV was designed to yield new information on the physics and mechanics of hypervelocity breakup. DebrisLV was designed in close collaboration with NASA and the Hypervelocity Impact expert-experimentalists at the Arnold Engineering Development Complex (AEDC) at Arnold AFB in order to represent the full-scale hypervelocity impact behavior of the current population of derelict launch vehicle upper stages in orbit. Although substantial forensic analysis remains to be done, the DebrisLV test has been extraordinarily fruitful in yielding new understanding of hypervelocity impacts.


Descriptors :   *FRAGMENTATION , *HYPERSONIC VELOCITY , *LAUNCH VEHICLES , HYPERVELOCITY IMPACT , LABORATORIES , MECHANICS , PHYSICAL PROPERTIES , TARGETS , TEST AND EVALUATION


Subject Categories : Explosions
      Fluid Mechanics
      Unmanned Spacecraft


Distribution Statement : APPROVED FOR PUBLIC RELEASE