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Delivered in late 1959, the K-16B underwent extensive wind tunnel testing, along with some tethered hops, to evaluate the tiltwing configuration's aerodynamic characteristics. Flight testing was originally anticipated to begin in the fall of 1960, however these preliminary tests continued into 1962.
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and other existing parts to reduce the cost and time necessary. The fuselage and tail of the Goose were mated to a new tilting wing and engine configuration; the maximum
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allowed was only 50 degrees; the rotorprop was expected to provide sufficient thrust to allow VTOL operations despite the low angle.
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concept for aircraft, with multiple experimental types ordered to develop the technology for potential service. The
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That year the project was cancelled with the aircraft having not conducted its first free flight.
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1959–1960 and the New
England Air Museum. All performance data estimated.
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134:, but was not flown before the project was terminated in 1962.
460:"Kaman K-16 in 40x80 Foot Wind Tunnel at Ames Research Center"
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3-bladed Kaman, 14 ft 10 in (4.5 m) diameter
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During the late 1950s, there was extensive interest in the
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Aircraft of comparable role, configuration, and era
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466:. NASA Ames Research Center. 19 September 1962
357:List of military aircraft of the United States
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290:200 mph (321.9 km/h, 173.8 kn)
296:250 mi (402.3 km, 217.24 nmi)
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832:1950s United States experimental aircraft
522:. London: Sampson Low, Marston & Co.
520:Jane's All the World's Aircraft 1959-1960
182:The prototype K-16B is on display at the
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126:amphibian, the K-16B underwent extensive
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202:The K-16B at the New England Air Museum
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537:Vertical Flight Aircraft of the World
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437:. Windsor Locks, CT. Archived from
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238:34 ft 0 in (10.36 m)
232:38 ft 4 in (11.68 m)
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539:. Fallbrook, CA: Aero Publishers.
244:19 ft 2 in (5.84 m)
150:contracted with Kaman Aircraft of
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110:aircraft that was constructed by
33:The K-16B with wing at full tilt
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256:8,000 lb (3,628.74 kg)
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852:Twin-turboprop tractor aircraft
302:16,000 ft (4,876.8 m)
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1:
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250:6,500 lb (2,948 kg)
704:HU2K/UH-2/HH-2/SH-2 Seaprite
535:Swanborough, Gordon (1964).
144:vertical takeoff and landing
108:vertical-takeoff-and-landing
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847:Turboshaft-powered aircraft
488:McGowen, Stanley S (2005).
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264:General Electric YT58-GE-2A
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269:, 1324.9 hp (988 kW) each
188:Windsor Locks, Connecticut
122:concept. Converted from a
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118:in 1959 to evaluate the
387:Swanborough 1964, p.50.
330:Canadair CL-84 Dynavert
217:General characteristics
152:Bloomfield, Connecticut
761:designations 1946-1962
435:New England Air Museum
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184:New England Air Museum
138:Design and development
759:experimental aircraft
709:SH-2G Super Seasprite
682:Military designations
496:. Santa Barbara, CA:
362:List of VTOL aircraft
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41:Experimental tiltwing
611:Company designations
568:at Wikimedia Commons
413:McGowen 2005, p.180.
106:was an experimental
312:Related development
169:Operational history
156:Grumman JRF-5 Goose
842:High-wing aircraft
318:Grumman G-21 Goose
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178:Surviving aircraft
163:angle of incidence
148:United States Navy
116:United States Navy
95:Grumman G-21 Goose
73:United States Navy
69:Primary user
837:Tiltwing aircraft
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564:Media related to
516:Taylor, John W.R.
404:1959–1960, p.331.
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441:on 2021-06-21
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431:"Kaman K-16B"
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351:Related lists
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254:Gross weight:
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248:Empty weight:
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124:Grumman Goose
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699:HH-43 Huskie
668:K-1200 K-Max
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468:. Retrieved
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443:. Retrieved
439:the original
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80:Number built
566:Kaman K-16B
345:Vertol VZ-2
335:Hiller X-18
281:Performance
273:Propellers:
267:turboshafts
260:Powerplant:
128:wind tunnel
104:Kaman K-16B
821:Categories
545:B009FNYH16
528:B002G60XF8
470:2017-12-02
445:2017-12-02
368:References
340:LTV XC-142
373:Citations
236:Wingspan:
207:Data from
159:amphibian
757:US Navy
605:aircraft
518:(1960).
498:ABC-CLIO
307:See also
120:tiltwing
114:for the
776:D-558-2
771:D-558-1
673:KSA-100
242:Height:
230:Length:
663:K-1125
543:
526:
504:
402:Jane's
294:Range:
210:Jane's
19:K-16B
801:V-173
796:M-270
791:K-225
786:K-16B
658:K-700
653:K-600
648:K-240
643:K-225
638:K-190
633:K-125
603:Kaman
224:Crew:
38:Role
806:Y2-2
781:L-39
716:Q-24
694:H-22
628:K-20
623:K-17
618:K-16
541:ASIN
524:ASIN
502:ISBN
262:2 ×
130:and
102:The
186:in
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418:^
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Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
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