Statistics – Applications
Scientific paper
Jan 2007
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2007aipc..880..579m&link_type=abstract
SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM-STAIF 2007: 11th Conf Thermophys.Applic.in Micrograv.; 24th Symp Space Nuc
Statistics
Applications
Spaceborne And Space Research Instruments, Apparatus, And Components
Scientific paper
As part of the Pluto New Horizons mission's safety effort, assessment of accidental ground impacts of the spacecraft (SC) and its components, including the radioisotope thermoelectric generator (RTG), near the launch pad are of particular interest as they determine the severity of the mechanical insult to the hardware. Two configurations are studied: the SC with RTG joined to the third stage STAR™ 48B solid rocket motor [Launch Vehicle (LV) payload], and the RTG joined to the RTG mounting fixture but separated from the SC after an at-altitude destruct action. The objective of the analyses conducted is to determine the probabilities of impact orientation and average impact velocity of these configurations for a near launch pad accident These are of interest because of the possibility that the STAR 48B solid rocket motor could impact on top of the RTG, and because the RTG/RTG mounting fixture impact orientations probabilities and velocities directly affect the mechanical response of the internal GPHS modules. The probabilities of impact orientation and impact velocity of the LV payload as a function of mission elapsed time at thrust termination are determined using a six degree of freedom motion simulation computer program coupled with a Monte Carlo method. The motion simulation accounts for the LV payload aerodynamic properties, mass properties, and the initial flight conditions (αt, γ, V, q and r). Baseline conditions for position, direction, velocity and angular rates, are obtained from the mission timeline information for the Atlas V 551 launch vehicle. The results from this new and unique approach contributed information to safety assessments for the launch approval process. As the environments associated with the RTG/RTG mounting fixture impact orientations probabilities and velocities were less severe than earlier assumptions, this contributed to a reduction in the estimated risk for the Pluto mission.
Chang Yale
Frostbutter Dave A.
McGrath Brian E.
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