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A contract for three MC-1 gliders, two flyable and one for static testing, was given to the
Airborne and General aircraft company, which had been formed by Bowlus and Criz. This company soon transformed into the General Airborne Transport company, which built the full sized MC-1 gliders with the
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In spite of all the design problems and the MC-1 crash, a contract was approved on 13 November 1943 for two test flight articles and one static test article of the MC-1 glider designated as the USAAF XCG-16. Only one XCG-16, (44-76193), was manufactured and tested, demonstrating good flying
164:, special assistant to Gen. Hap Arnold; Col. Ernest Gabel, another glider specialist on the staff of the Chief of Staff of the Air Force, and C. C. Chandler, thrice soaring champion aboard. Inadequately secured ballast came loose when the glider flew through the
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qualities, but major issues with military equipment and procedures precluded the CG-16 from a production contract, as it did not meet military expectations as a combat glider. The contract for all remaining work on the CG-16 was cancelled on 30 November 1944.
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Three prototypes of the military XCG-16 were ordered, but only one was completed as 44-76193. Trials revealed major deficiencies in the ability of the CG-16 to fulfill the intended mission, despite good flying
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A flying 1:2 scale model of the MC-1/XCG-16. Successful flight trials proved the aerodynamic qualities of the MC-1. After completion of CG-16 related flying the 1:2 scale MC-1 was converted to a flying wing by
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To prove the concept and aerodynamic qualities Bowlus designed a 1:2 scale prototype, which flew successfully. The flight tests of the 1:2 scale MC-1 maintained confidence in the full-sized glider.
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laid out in U.S. Patent No. 1,758,498, issued on 13 May 1930, which advocated the use of "lifting fuselages" providing a high proportion of the total lift. To enter a competition at
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Flight tests of the full sized MC-1, registered to the Albert Criz company on 19 July 1943 as NX21757, commenced at
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The full-scale civilian prototype of the CG-16, destroyed on its second flight during a demonstration flight.
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and Albert Criz designed a
Burnelli style lifting fuselage assault glider as the Bowlus-Criz MC-1.
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The end of Forked Ghosts: Twin-tail-boom aircraft designs of 1939-45 — Facts and
Fantasy
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176:. Three of the crew and passengers jumped out, but only two survived the parachute jump.
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Design of the CG-16 evolved from the lifting fuselage theories of
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was a military transport/assault glider ordered by the
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detailed article with photos and drawings, June 1945
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1113:1940s United States military transport aircraft
122:. The XCG-16’s preferred tow aircraft was the
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412:. www.twitt.org. 2002-07-13. Archived from
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262:42 troops or 10,050 lb (4,570 kg) of cargo
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322:220 mph (354 km/h, 190 kn)
542:glider aircraft designations 1924–1962,
142:for a new assault glider for the USAAF,
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354:. www.indianamilitary.org. 2010-09-27
83:1x 1/2 scale MC-1, 1x MC-1, 1x XCG-16
7:
1123:1940s United States military gliders
286:1,139 sq ft (105.9 m)
274:91 ft 10 in (27.98 m)
492: — with photos and description
352:"General Airborne Transport XCG-16"
268:48 ft 4 in (14.72 m)
280:18 ft 4 in (5.58 m)
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221:General Airborne Transport XCG-16
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307:19,540 lb (8,880 kg)
114:, for competition against the
112:General Airborne Transport Co.
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301:9,480 lb (4,310 kg)
153:military designation XCG-16.
108:United States Army Air Forces
1128:Aircraft first flown in 1943
410:"Don Mitchell Autobiography"
41:The XCG-16 flying over Ohio.
200:Bowlus-Criz MC-1 half-scale
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496:Don Mitchell autobiography
456:Don Mitchell autobiography
162:Richard Chichester du Pont
124:Lockheed Model 18 Lodestar
74:General Airborne Transport
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546:designations 1962–present
215:Airborne and General MC-1
55:Military transport glider
34:
941:1948 USAF redesignations
247:General characteristics
195:XCG-16 in October, 1944
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130:Design and development
552:USAAC/USAAF sequences
442:Glides at 200 M.P.H."
373:U.S. patent 1,758,498
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997:Tri-Service sequence
241:indianamilitary.org
47:General information
1118:Twin-boom aircraft
478:2012-02-05 at the
461:2012-03-12 at the
388:. www.burnelli.com
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210:Bowlus Sailplanes
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96:11 September 1943
16:(Redirected from
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473:Aircrash: XCG-16
451:Burnelli history
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446:Popular Science
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60:National origin
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735:Powered glider
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561:Assault glider
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432:External links
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320:Maximum speed:
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233:Specifications
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490:XCG-16 Glider
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416:on 2012-03-12
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305:Gross weight:
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299:Empty weight:
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166:Lockheed C-60
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144:Hawley Bowlus
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63:United States
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1095:Not assigned
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608:Cargo glider
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418:. Retrieved
414:the original
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356:. Retrieved
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291:Aspect ratio
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206:Don Mitchell
182:
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168:tow plane's
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140:Wright Field
133:
120:Wright Field
103:
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93:First flight
80:Number built
69:Manufacturer
719:Fuel glider
582:Bomb glider
554:(1924–1947)
544:Tri-Service
468:Уголок неба
313:Performance
158:March Field
1107:Categories
438:"42 Place
420:2011-06-21
392:2011-06-21
386:"Burnelli"
358:2011-06-21
329:References
284:Wing area:
256:Two pilots
225:qualities.
116:Waco CG-13
272:Wingspan:
260:Capacity:
238:Data from
174:flat spin
476:Archived
459:Archived
187:Variants
170:propwash
278:Height:
266:Length:
88:History
18:XCG-16A
104:XCG-16
30:XCG-16
1076:G-15A
928:TG-33
923:TG-32
918:TG-31
913:TG-30
908:TG-29
903:TG-28
898:TG-27
893:TG-26
888:TG-25
883:TG-24
878:TG-23
873:TG-22
868:TG-21
863:TG-20
858:TG-19
853:TG-18
848:TG-17
843:TG-16
838:TG-15
833:TG-14
828:TG-13
823:TG-12
818:TG-11
813:TG-10
710:CG-20
705:CG-19
700:CG-18
695:CG-17
690:CG-16
685:CG-15
680:CG-14
675:CG-13
670:CG-12
665:CG-11
660:CG-10
536:USAAF
532:USAAC
254:Crew:
118:A at
1085:G-16
1071:G-14
1066:G-13
1061:G-12
1056:G-11
1051:G-10
988:G-20
983:G-18
978:G-15
973:G-14
968:G-13
963:G-10
808:TG-9
803:TG-8
798:TG-7
793:TG-6
788:TG-5
783:TG-4
778:TG-3
773:TG-2
768:TG-1
752:PG-3
747:PG-2
742:PG-1
726:FG-1
655:CG-9
650:CG-8
645:CG-7
640:CG-6
635:CG-5
630:CG-4
625:CG-3
620:CG-2
615:CG-1
599:BG-3
594:BG-2
589:BG-1
573:AG-2
568:AG-1
540:USAF
440:Wing
102:The
52:Type
1046:G-9
1041:G-8
1036:G-7
1031:G-6
1026:G-5
1021:G-4
1016:G-3
1011:G-2
1006:G-1
958:G-4
953:G-3
948:G-2
295:7.4
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401:^
337:^
126:.
1080:B
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524:e
517:t
510:v
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361:.
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20:)
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