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The system must operate without any need for aircraft power or other interactions. The system should not add more than one pound of aircraft weight per occupant.
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PHASE I: Perform a design study to support of the development of a system that will integrate seamlessly with existing crash worthy aircraft systems on rotary wing and fixed wing military aircraft.
Conduct an assessment of appropriate technologies which may be utilized to build, integrate, and test a system to meet the challenges listed above.
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It is also the political centre of the country, as its seat of Government and residence of the Head of State.Verify aircraft suitability by testing to MIL-STD-810 or FAA TSO 8043 requirements for safe to fly status on selected aircraft.PHASE III: The innovation developed under this topic can be offered as a tested and qualified solution to improve crash safety across military and FAA aircraft.DESCRIPTION: Current Military Helicopters and Fixed Wing Aircraft use occupant safety systems based on older technologies.These older systems may not always adequately address occupant extreme movement during crash or hard landings.The official link for this solicitation is: https://osd.mil/osbp/sbir/solicitations/index.shtml TECHNOLOGY AREA(S): Air Platform OBJECTIVE: Develop air platform occupant safety improvements to prevent injury or fatality within the constraints associated with legacy air vehicles.