All large spacecraft are susceptible to high-speed impacts by meteoroi
ds and pieces of orbiting space debris which can damage flight-critica
l systems and in turn lead to catastrophic failure. One way to obtain
information on the response of a structure to a meteoroid impact or an
orbital debris impact is to simulate the impact conditions of interes
t in the laboratory and analyze the resulting damage to a target struc
ture. As part of the Phase B and C/D development activities for the Sp
ace Station Freedom, 950 impact tests were performed using the NASA/Ma
rshall Space Flight Center (MSFC) light gas gun from 1985-1991. This p
aper presents the results of impact phenomena repeatability and data u
ncertainty studies performed using the information obtained from those
tests. The results of these studies can be used to assess the utility
of individual current and future NASA/MSFC impact test results in the
design of long-duration spacecraft.