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Hypersonic Technology Vehicle 2 (HTV-2) is a crewless, experimental hypersonic glide vehicle rocket glider developed as part of the DARPA Falcon Project capable of flying at 13,000 mph (21,000 km/h). It is a test bed for technologies to provide the United States with the capability to reach any target in the world within one hour using an unmanned hypersonic bomber aircraft.
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Development
The Falcon HTV-1 program, which preceded the Falcon HTV-2 program, was conducted in April, 2010. The mission ended within nine minutes from launch. Both these missions are funded by the US Defense Advanced Research Projects Agency (DARPA) to help develop hypersonic technologies and to demonstrate its effectiveness. Under the original plan, HTV-1 was to feature a hypersonic lift-to-drag ratio (L/D) of 2.5, increasing to 3.5-4 for the HTV-2 and 4-5 for the HTV-3. The actual ratio of HTV-2 was estimated to be 2.6.
HTV-2 was to lead to the development of an HTV-3X vehicle, known as Blackswift, which would have formed the basis for deployment around 2025 of a reusable Hypersonic Cruise Vehicle, an unmanned aircraft capable of taking off from a conventional runway with a 5,400 kg (12,000 lb) payload to strike targets 16,650 km away in under 2h. The HCV would have required an L/D of 6-7 at M10 and 130,000 ft (40,000m).
Design
Development of protection structures that are tough and light-weight, development of an aerodynamic shape that has a high lift to drag ratio, development of automatic navigation control systems etc. were some of the initial technical challenges that had been overcome in the final design. The various departments involved in designing the vehicle included aerothermodynamics, materials science, hypersonic navigation, guidance and control systems, endo- and exo-atmospheric flight dynamics, telemetry and range safety analysis. The craft could cover 17,000 kilometres, the distance between London and Sydney, in 49 minutes.
Flight testing
The HTV-2's first flight was launched on 22 April 2010. The HTV-2 glider was to fly 4,800 miles (7,700 km) across the Pacific to Kwajalein at Mach 20. The HTV-2 was boosted by a Minotaur IV Lite rocket launched from Vandenberg Air Force Base, California. The flight plan called for the craft to separate from the launch vehicle, level out and glide above the Pacific at Mach 20. Contact was lost with the vehicle nine minutes into the 30-minute mission. In mid-November, DARPA stated that the first test flight ended when the computer autopilot "commanded flight termination" after the vehicle began to roll violently.
A second flight was initially scheduled to be launched on August 10, 2011, but bad weather forced a delay. The flight was launched the following day, on 11 August 2011. The unmanned Falcon HTV-2 successfully separated from the booster and entered the mission's glide phase, but again lost contact with control about nine minutes into its planned 30-minute Mach 20 glide flight. Initial reports indicated it purposely impacted the Pacific Ocean along its planned flight path as a safety precaution.
Future development
DARPA does not plan to conduct a third flight test of the HTV-2. The decision was made because substantial data was collected from the first two flights, and a third was not thought likely to provide any additional valuable data for the cost. The first flight provided data in aerodynamics and flight performance, while the second provided information about structures and high temperatures. Experience gained from the HTV-2 will be used to improve hypersonic flight.
Work on the HTV-2 will continue to Summer 2014 to capture technology lessons and improve design tools and methods for high-temperature composite aeroshells.