A system and method for collecting test data from a unit under test (UUT) in a multi-gravity environment is disclosed. In one embodiment, the method comprises determining a desired accelerative load profile for the UUT, determining the commanded flight profile of a flight vehicle at least in part from the desired accelerative load profile and a predicted dynamic response of the flight vehicle having the UUT mounted thereto to the commanded flight profile, commanding the flight vehicle having the UUT mounted thereto to fly the determined flight profile, and collecting the test data using a data acquisition system communicatively coupled to the UUT.