Grumman X-29

 

Podatki iz NASA X-Planes

Splošne karakteristike

• Posadka: 1 pilot
• Tovor: 4000 lb (1810 kg)
• Dolžina: 48 ft 1 in (14,7 m)
• Razpon kril: 27 ft 2 in (8,29 m)
• Višina: 14 ft 9 in (4,26 m)
• Površina kril: 188,8 ft² (17,54 m²)
• Teža praznega letala: 13800 lb (6260 kg)
• Maks. vzletna teža: 17800 lb (8070 kg)
• Pogon letala: 1 × General Electric F404 turbofan, 16000 lbf (71,2 kN)

Zmogljivost

• Maks. hitrost: Mach 1.8 (1100 mph, 1770 km/h na 33000 čevljih (10000 m))
• Doseg: 350 milj (560 km)
• Višina leta: 55000 ft (16800 m)

• Krilo z negativnim naklonom
• Northrop F-5
• Suhoj Su-47

• Butts, S. L.; Hoover, A. D. (Maj 1989). »Flying Qualities Evaluation of the X-29A Research Aircraft«. U.S. Air Force Flight Test Center. AFFTC-TR-89-08. {{navedi revijo}}: Sklic magazine potrebuje|magazine= (pomoč)
• Donald, David, ur. (1997). »Grumman X-29A«. The Complete Encyclopedia of World Aircraft. New York: Barnes & Noble. ISBN 0-7607-0592-5.
• Green, William (1970). Warplanes of the Third Reich. New York: Doubleday. ISBN 0-385-05782-2.
• Jenkins, Dennis R.; Landis, Tony; Miller, Jay (Junij 2003). American X-Vehicles: An Inventory—X-1 to X-50 (PDF). Monographs in Aerospace History No. 31. NASA. OCLC 68623213. SP-2003-4531.
• Pamadi, Bandu N. (2004). Performance, Stability, Dynamics, and Control of Airplanes (2. izd.). American Institute of Aeronautics and Astronautics. doi:10.2514/4.862274. ISBN 978-1-56347-583-2.
• Putnam, Terrill W. (Januar 1984). X-29 Flight-Research Program (PDF). AIAA 2nd Flight Test Conference. Las Vegas, Nevada. 16-18 November 1983. NASA. TM-86025.
• Roskam, Jan (1985). Airplane Design, Part II: Preliminary Configuration Design and Integration of the Propulsion System. Ottawa, Kansas: Roskam Aviation and Engineering Corporation. ISBN 978-1-88488-543-3.
• Thruelsen, Richard (1976). The Grumman Story. New York: Praeger Publishers. ISBN 0-275-54260-2.
• Treadwell, Terry (1990). Ironworks: Grumman's Fighting Aeroplanes. Shrewsbury, UK: Airlife Publishers. ISBN 1-85310-070-6.
• Warwick, Graham (16. junij 1984). »Forward-sweep Technology«. Flight International: 1563–1568.
• Webster, Frederick R.; Purifoy, Dana (Julij 1991). X-29 High Angle-of-Attack Flying Qualities. U.S. Air Force Flight Test Center. AFFTC-TR-91-15. Arhivirano iz prvotnega spletišča dne 26. avgusta 2014. Pridobljeno 3. novembra 2014.
• Winchester, Jim (2005). »Grumman X-29«. X-Planes and Prototypes. London: Amber Books. ISBN 1-904687-40-7.

 

Wikimedijina zbirka ponuja več predstavnostnega gradiva o temi: Grumman X-29.

• Fact Sheet: Grumman X-29 at NASA.gov
• Fact Sheet: Grumman X-29A by the National Museum of the U.S. Air Force
• Grumman X-29 Photo Collection at NASA.gov
• Grumman X-29 Movie Collection Arhivirano 2015-07-21 na Wayback Machine. at NASA.gov
• X-29: Aircraft with Forward Swept Wings (part 1, part 2) at Military.com