Forward Bay Cover Separation Modeling and Testing for the Orion Multi-Purpose Crew Vehicle

摘要

Spacecraft multibody separation events during atmospheric descent require complex testing and analysis to validate the flight separation dynamics model and to verify no recontact. NASA Orion MultiPurpose Crew Vehicle (MPCV) teams examined key model parameters and risk areas to develop a robust but affordable test campaign in order to validate and verify the Forward Bay Cover (FBC) separation event for Exploration Flight Test1 (EFT1). The FBC jettison simulation model is highly complex, consisting of dozens of parameters varied simultaneously, with numerous multiparameter interactions (coupling and feedback) among the various model elements, and encompassing distinct nearfield, midfield, and farfield regimes. The test campaign was composed of componentlevel testing (for example gaspiston thrusters and parachute mortars), ground FBC jettison tests, and FBC jettison airdrop tests that were accomplished by a highly multidisciplinary team. Three ground jettison tests isolated the testing of mechanisms and structures to anchor the simulation models excluding aerodynamic effects. Subsequently, two airdrop tests added aerodynamic and parachute parameters, and served as integrated system demonstrations, which had been preliminarily explored during the Orion Pad Abort1 (PA1) flight test in May 2010. Both ground and drop tests provided extensive data to validate analytical models and to verify the FBC jettison event for EFT1, but more testing is required to support human certification, for which NASA and Lockheed Martin are applying knowledge from Apollo and EFT1 testing and modeling to develop a robust but affordable human spacecraft capability.