- Joined
- 6 August 2007
- Messages
- 3,344
- Reaction score
- 3,463
I'm surprised this does not already have a topic.
HAVE SLICK was the Advanced Dispenser Weapon Technology program. The HAVE SLICK dispenser was a 2000lb-class conformal, stealthy standoff/cruise missile to be integrated with LO launch aircraft. HAVE SLICK was flight tested at Eglin AFB in 1989, program management was by the Eglin Armament Lab under Col. William O'Brien
From:
http://www.iste.uni-stuttgart.de/ps/AdaBasis/pal_1195/ada/asr/ptrs/atipf88.inf
Known papers:
“Winchenbach,G.L., Stephens,M., Hathaway,W.H., Whyte,R.H., Aerodynamic Test Results: Have Slick Configurations, WL/MN-TR-91-78, September 1991.”
http://www.prodas.com/XQ/ASP/P.102/QX/webPageXML4.htm
(I have not been able to get the paper yet)
Budget documents:
DEPARTMENT OF DEFENSE IN-HOUSE RDT&E ACTIVITIES
http://www.dtic.mil/cgi-bin/GetTRDoc?Location=U2&doc=GetTRDoc.pdf&AD=ADA240847
Will update later with the PE code when I find it in paper archives.
AvWeek at one point published a photo with a conformal shape under an F-111 that was labelled as HAVE SLICK.
This may be a final HAVE SLICK configuration:
http://up-ship.com/blog/?p=7088
HAVE SLICK was the Advanced Dispenser Weapon Technology program. The HAVE SLICK dispenser was a 2000lb-class conformal, stealthy standoff/cruise missile to be integrated with LO launch aircraft. HAVE SLICK was flight tested at Eglin AFB in 1989, program management was by the Eglin Armament Lab under Col. William O'Brien
From:
http://www.iste.uni-stuttgart.de/ps/AdaBasis/pal_1195/ada/asr/ptrs/atipf88.inf
HAVE SLICK
This program will develop and flight test a 2000 pound class standoff dispenser weapon airframe. The airframe has an asymmetric cross-section to maximize the dispenser's aerodynamic performance. This unique design also allows for very low incarriage drag which improves aircraft performance. The flight control software for real-time guidance, navigation and control subsystems will be written in Ada and executed on a 1750A based microprocessor.
Known papers:
“Winchenbach,G.L., Stephens,M., Hathaway,W.H., Whyte,R.H., Aerodynamic Test Results: Have Slick Configurations, WL/MN-TR-91-78, September 1991.”
http://www.prodas.com/XQ/ASP/P.102/QX/webPageXML4.htm
(I have not been able to get the paper yet)
Budget documents:
DEPARTMENT OF DEFENSE IN-HOUSE RDT&E ACTIVITIES
http://www.dtic.mil/cgi-bin/GetTRDoc?Location=U2&doc=GetTRDoc.pdf&AD=ADA240847
Will update later with the PE code when I find it in paper archives.
AvWeek at one point published a photo with a conformal shape under an F-111 that was labelled as HAVE SLICK.
This may be a final HAVE SLICK configuration:
http://up-ship.com/blog/?p=7088