Directory of U.S. Military Rockets and Missiles Appendix 4: Undesignated Vehicles |
HAVE DASH II |
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Copyright © 2003-2005 Andreas Parsch |
Note: I don't have any first-hand printed sources on HAVE DASH available. Therefore I had to rely on Internet sources (q.v. under "Main Sources" below), which may or may not be accurate. However, it has been indicated by someone who was involved with the program, that the information is essentially correct.
In the early 1990s, the USAF studied advanced air-to-air missile technologies under the HAVE DASH program. It is not known if HAVE DASH (I) itself resulted in any flying hardware. However, in 1990 the Aeronutronics division of Ford Aerospace (which was later acquired by Loral) was awarded a contract to build flight-test missiles to evaluate technologies for a stealthy long-range air-to-air missile under the HAVE DASH II program. To ensure a low radar cross section (RCS), the HAVE DASH II design featured a radar-absorbing graphite composite fuselage with a flat-surfaced trapezoidal cross-section for the whole body except for the radome. Stability and control was provided by four tail fins. The shape allowed the missile to be carried externally flush on the carrier aircraft, thereby minimizing its attribution to total RCS. The stealthy missile would also be less detectable by the attacked aircraft's warning sensors.
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Image: (anonymous source, unknown origin) |
HAVE DASH II |
The shape of the HAVE DASH II missile provided additional body lift, and this, combined with the fin configuration and a new bank-to-turn autopilot, permitted maneuvering at 50g (versus 35g for "conventional" missiles). The missile was to use an inertial navigation system and a dual-mode (infrared/active-radar) seeker. The airframe was designed to accomodate an air-breating engine (most likely an integral rocket/ramjet), but the HAVE DASH II test vehicles were reportedly flown with solid-fueled MK 58 rocket motors of surplus AIM-7F/M Sparrow missiles.
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Drawing: Loral |
HAVE DASH II |
The HAVE DASH II program was apparently terminated after the flights of the test vehicles (most likely in the 1992/93 time frame). No reliable information about the level of success is available.
Note: Data given by several sources show slight variations. Figures given below may therefore be inaccurate!
Data for HAVE DASH II:
Length | 3.6 m (12 ft) |
Weight | 180 kg (400 lb) |
Speed | Mach 4 |
Range | 50 km (30 miles) |
Propulsion | MK 58 MOD 5 solid-fueled rocket |
Back to Directory of U.S. Military Rockets and Missiles, Appendix 4