Abstract
 Missile and space-vehicle performance histories contain many examples of failures that
 cause, or have the potential to cause, significant vehicle deviations from the intended
 flight line. In RTI's risk-analysis program, DAMP, such failures are referred to as
 Mode-5 failure responses. Although Mode-5 failure responses are much less likely to
 occur than those that result in impacts near the flight line, risk-analysis studies are
•incomplete without them. This report shows how impacts from Mode-5 failures are
 modeled in program DAMP. The impact density function used for this purpose
 contains two shaping constants that control the rate at which the density function drops
 in value as the angular deviation from the flight line and the impact range increase.
 Certain Mode-5 malfunctions are simulated, and the two shaping constants then chosen
 by trial and error so that impacts from the simulated malfunctions and the theoretical
 density function are in close agreement.
An appendix to the report contains a listing and brief narrative failure history of the
Atlas, Delta, and Titan missile and space-vehicle launches from the Eastern and
Western Ranges from the beginning of each program through August 1996. Each entry
gives the vehicle configuration, whether the flight was a success, the flight phase in
which any anomalous behavior occurred, and a classification of vehicle behavior in
accordance with defined failure-response modes. Various filtering or data weighting
techniques are described. The empirical data are then filtered to estimate (1) failure
probabilities for Atlas, Delta, and Titan, and (2) percentages of future failures that will
result in Mode-5 (and other Mode) responses.




9/10/96                                                                                RTI