Phase 2-A full scale, approximate X-24A shape without outboard fins and low-cost mockups. These will include parachute controls but no active vehicle
control systems or aerodynamic surfaces (inert). These vehicles will be dropped from a C-130 at the Army test facility at Yuma, Arizona.
- Demonstrate deployment, autonomous flight, and landing flare
capability of a parafoil/payload system with a wing loading of 2.0 pounds per
square foot.
- Make a preliminary evaluation of the touchdown dynamics of the
full-scale vehicle/parachute combination.
- Measure stability and control of the full-scale vehicle/parachute combination.
- Demonstrate integration and operation (including guidance) of the Guided Precision Aerial Delivery System (GPADS) parachute recovery
system. This system has been developed by Pioneer Corporation under
contract to the US. Army for use in the delivery of military equipment
to specific target areas.
- Begin assessment of parachute system reliability.
- Measure parafoil riser and ground impact loads for structural analysis.
- Demonstrate composite structure integrity.