DRS Sentry HP: Difference between revisions
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==References== |
==References== |
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This article contains material that originally came from the web article [http://www.vectorsite.net/twuav.html ''Unmanned Aerial Vehicles''] by Greg Goebel, which exists in the Public Domain. |
This article contains material that originally came from the web article [https://web.archive.org/web/20110902194407/http://www.vectorsite.net/twuav.html ''Unmanned Aerial Vehicles''] by Greg Goebel, which exists in the Public Domain. |
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* [http://www.janes.com/extracts/extract/juav/juav0745.html ''Jane's Unmanned Aerial Vehicles and Targets''] |
* [http://www.janes.com/extracts/extract/juav/juav0745.html ''Jane's Unmanned Aerial Vehicles and Targets''] |
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* [http://www.drs.com/Products/SENTRY.aspx?cat=Intel_Tech&subcat=Sub_Cat_22 Manufacturer's website] |
* [http://www.drs.com/Products/SENTRY.aspx?cat=Intel_Tech&subcat=Sub_Cat_22 Manufacturer's website] |
Revision as of 23:41, 20 July 2016
Sentry HP | |
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Sentry HP at the 2010 Farnborough Airshow | |
Role | Reconnaissance UAV |
National origin | United States |
Manufacturer | DRS Technologies |
The DRS Sentry HP is a reconnaissance UAV that was developed in the United States in the late 1980s by S-TEC. The program was acquired by Meggitt in 2000 and subsequently by DRS in 2002. Although the aircraft shares the name "Sentry" with a previous S-TEC design, the Sentry HP is a completely different machine, with a broad wing and a vee tail. The Sentry HP is larger, with greater payload capacity and an underwing stores capability. It is powered by a variant of the same engine as the Sentry. It can be ordered with an option for fixed landing gear to permit conventional takeoff and recovery.
Specifications
General characteristics
- Crew: None
- Capacity: 75 lb (34 kg) payload
Performance
References
This article contains material that originally came from the web article Unmanned Aerial Vehicles by Greg Goebel, which exists in the Public Domain.