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Republic XF-12 Rainbow

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199:. Both were powered by the new P&W R-4360. The XF-12's first flight was made on 4 February 1946 and during flight testing, it reached an altitude of 45,000 ft (14,000 m) at 470 mph (760 km/h), and demonstrated a range of 4,500 mi (7,200 km), exceeding design criteria. The XF-12 could photograph in both daylight and night and under conditions of reduced visibility at high altitudes over long ranges and with great speed. This "flying photo lab" was capable of mapping broad stretches of the globe. 224: 322:
aircraft and reduce the risk of fire. The pilot landed on the left main gear and the nose wheel and despite losing as much speed as possible before the other wing dropped, the aircraft suffered significant damage. The wing spar was cracked, and engines and props needed to be replaced but it was repaired by Republic, and returned to service. When the U.S. Army Air Forces became the U.S. Air Force the XF-12 was later re-designated
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prevent frost build-up. The XF-12 also carried complete darkroom facilities to permit developing and printing the film while still airborne augmented by adjustable storage racks to handle any size of film container and additional photo equipment. This allowed immediate access to the intelligence after landing without the usual processing delay.
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made tentative orders, but without military F-12 orders to subsidize development and tooling costs, the RC-2's purchase price was higher than they would accept. The RC-2 also would have had higher operating costs per passenger than more capacious airliners with similar fuel consumption such as the
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boost for increased power at high speeds, and more effective cooling of the oil and intercoolers. The intakes made up 25% of the total wingspan and were extensively wind tunnel tested. After being used, the air was ducted toward the rear of the nacelle, to provide thrust. The entire engine nacelle
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K-17 camera. For night reconnaissance, the XF-12 had a belly hold which accommodated 18 high-intensity photo-flash bombs to be ejected over the target. All bays were equipped with electrically operated, inward retracting doors designed for minimum drag and camera lenses were electrically heated to
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from a photographic suitability test flight after the number 2 (port inner) engine exploded, causing violent buffeting. Five of the seven crew escaped safely while two crew members were killed. The first prototype continued flight testing after being returned to service in 1948 but with no orders
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The first prototype was damaged on 10 July 1947 while undergoing maximum landing weight tests when the right main gear was severed at the engine nacelle. After bouncing hard and staggering back into the air the test pilot climbed to a safe altitude where excess fuel was burnt off, to lighten the
176:, due to the range requirements of operating in the Pacific, existing fighters and bombers were being used but were poorly suited to the USAAF's needs. The requirement existed for dedicated photo-reconnaissance aircraft with speed, range, and altitude capabilities beyond what was then available. 167:
Air Technical Service Command in late 1943 was for a 400 mph (640 km/h) reconnaissance aircraft with a range of 4,000 nmi (7,400 km; 4,600 mi) and a ceiling of 40,000 ft (12,000 m). Its primary objective was high-speed overflights of the
143:. The XF-12 was referred to as "flying on all fours" meaning: four engines, 400 mph (640 km/h) cruise, 4,000 mi (6,400 km) range, at 40,000 ft (12,000 m). The aircraft was designed to maximize aerodynamic efficiency. Although innovative, the 304:
similar to those used on the XF-11, However, due to delivery delays and reliability issues, they were never installed. They would have been twinned three-bladed propellers (rotating in opposite directions). As it was, the aircraft used standard four-bladed
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before heading east. It then photographed its entire flight path across the United States on 390 individual 10 in (250 mm) photos each covering 490 mi (790 km), which were jointed to form a continuous 325 ft (99 m) print.
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of each wing between the inboard and outboard engines. This reduced drag compared to using individual intakes for each component. In addition, because the air was taken from a high-pressure area at the front of the wing, this provided a
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hub. These refinements allowed the engines to be tightly cowled for aerodynamic efficiency, while still keeping the engines adequately cooled. When the sliding cowl ring was closed during flight, the cooling air was ducted through the
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Minimizing drag was a primary consideration throughout the design of the XF-12. Many features came from Republic's experience with fighter aircraft. Unusually, no compromises to the aerodynamics were made in the shape of its
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each would replace the R-4360-31s, providing more power at lower altitudes, and fuel capacity would be increased. The airliner would carry a crew of seven, and the lavishly appointed cabin for 46 passengers would feature
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forthcoming and with the second prototype lost, flight testing was wound down and the remaining prototype was retired in June 1952, having flown just 117 hours from 1949 to 1952. It was later expended as a target at the
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The only visible external difference between the first and second prototypes was the addition of cooling gills on the upper engine cowlings. The second prototype was fitted with the full reconnaissance equipment suite.
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Only two prototypes were built each of the XF-11 and the XF-12 were ordered into service by the U.S. Army Air Forces, as the requirement evaporated after World War II ended, while the cheaper off-the-shelf
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to sea level with air conditioning, an electric galley providing hot meals, and an inflight lounge. The RC-2 would cruise above bad weather at 435 mph (700 km/h) at 40,000 feet (12,000 m).
289:. Research showed that a force roughly equivalent to 250 hp (190 kW) was generated by each engine exhaust during high speed cruise while at altitude. Each engine featured twin General Electric 352:, New York after six hours and 55 minutes at an average speed of 361 mph (581 km/h). A photo was taken approximately every 66 seconds. The flight was featured in the 29 November 1948 issue of 1825: 191:"recon" unit, recommended the acquisition of a dedicated high-performance photo reconnaissance aircraft to provide pre- and post-strike target analysis intelligence as well as 1815: 215:
entered service. The XF-12 was the fastest aircraft of its day to use four reciprocating engines, and the only one to exceed 450 mph (720 km/h) in level flight
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was quoted as saying "the sharp nose and cylindrical cigar shape of the XF-12 fulfills a designer's dream of a no compromise design with aerodynamic considerations."
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and the filmstrip exhibited at the 1948 U.S. Air Force Association Convention in New York. The XF-12 program had already been canceled when this flight was made.
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which could be readily converted into airliners for a fraction of the cost of new aircraft. Thus, the RC-2 program was cancelled before any were built.
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was conceived to demonstrate the XF-12's capabilities. On 1 September 1948, the second prototype departed the U.S. Air Force Flight Test Center at
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to facilitate engine cooling instead of cowling flaps, which caused too much drag. There was also a two-stage impeller fan directly behind the
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to better allow commanders to make decisions for bombing raids. Republic Aviation submitted the XF-12 and it was competing against the
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For its reconnaissance role, the XF-12 had three photographic compartments aft of the wing. One vertical, one split vertical, and one
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4-bladed Curtiss, 16 ft 1 in (4.9 m) diameter reversible-pitch constant-speed propellers
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nose replaced with a conventional nose. Pratt & Whitney R-4360-59s with only one General Electric
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to the rear exhaust orifice increasing thrust, rather than adding drag as is usually the case.
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World's Fastest Four-Engine Piston-Powered Aircraft: Story of the Republic XR-12 Rainbow
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made it obsolete, and it did not enter production. A proposed airliner variant, the
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400 mph (640 km/h, 350 kn) at 40,000 ft (12,000 m)
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Air for engine intakes, oil coolers and intercoolers was drawn through the
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Company in the late 1940s. Like most large aircraft of the era, it used
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at the rear of the nacelle and for brief bursts of additional power,
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On 7 November 1948, the second prototype crashed while returning to
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for maximum efficiency and squared tips. The engines used a sliding
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Luce, Henry R., ed. (29 November 1948). "Speaking of pictures".
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5,000 US gal (4,200 imp gal; 19,000 L)
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Marrett, George (December 2005). "Flights Into the Future".
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Cancelled military aircraft projects of the United States
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Machat, Mike (April 1994). "Somewhere, Under a Rainbow".
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could temporarily fill the role until the jet-powered
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1940s United States military reconnaissance aircraft
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Aircraft of comparable role, configuration, and era
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During 13: 889:"F-12 Based on fighter experience" 473:1,640 sq ft (152 m) 467:28 ft 4 in (8.63 m) 14: 1857: 1658:Strategic reconnaissance sequence 1500:designations, Army/Air Force and 863:. St. Paul, MN: Specialty Press. 16:Prototype reconnaissance aircraft 514:101,400 lb (45,994 kg) 27: 826: 785:Bridgman, Leonard, ed. (1947). 747: 600:8.4 lb/hp (5.1 kg/kW) 585:5,000 ft/min (25 m/s) 508:65,000 lb (29,484 kg) 179:In August 1943, U.S. President 163:The original proposal from the 1635:Reconnaissance/strike sequence 738: 579:44,000 ft (13,000 m) 158: 1: 1821:Four-engined tractor aircraft 648: 84:United States Army Air Forces 1841:Four-engined piston aircraft 1836:Aircraft first flown in 1946 1510:Army/Air Force main sequence 882:. Vol. 35, no. 12. 653: 530:28-cyl. four-row air-cooled 165:United States Army Air Corps 7: 854:. 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Roosevelt 46:aerial reconnaissance 1605:Prefix R-, 1947–1962 1519:Prefix F-, 1930–1947 364:Eglin Air Force Base 193:photo interpretation 699:Marrett, 2005, p.26 669:Marrett, 2005, p.23 330:Operation Birds Eye 317:Operational history 139:, specifically the 36:General information 1706:Converted fighters 775:Machat, 1994, p.51 744:Machat, 1994, p.50 735:Machat, 1994, p.10 726:Machat, 1994, p.14 717:Machat, 1994, p.16 687:Machat, 1994, p.12 229: 1846:Mid-wing aircraft 1831:Low-wing aircraft 1811:Republic aircraft 1798: 1797: 1794: 1793: 1742:Converted bombers 1630: 1629: 1463: 1462: 1135: 1134: 975:Republic aircraft 939:Seversky aircraft 803:Lednicer, David. 708:Machat, 1994, p.9 405:American Airlines 393:turbosupercharger 334:Muroc, California 187:, commander of a 170:Japanese homeland 133:Republic Aviation 118: 117: 66:Republic Aviation 1853: 1703: 1702: 1516: 1515: 1502:1962 Tri-Service 1490: 1483: 1476: 1467: 1466: 979: 978: 924: 917: 910: 901: 900: 896: 883: 874: 855: 846: 820: 819: 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Retrieved 808: 786: 780: 771: 762: 754: 749: 740: 731: 722: 713: 704: 683: 674: 636: 635: 621:Hughes XF-11 609: 608: 594: 588: 582: 576: 570: 565:Stall speed: 564: 558: 552: 545: 543: 537: 523: 517: 511: 505: 495: 489: 476: 470: 464: 458: 452: 446: 439: 437: 432: 431: 418:Douglas DC-6 403: 384: 382: 361: 354: 343: 329: 328: 323: 320: 311: 299: 277:leading edge 274: 257:aspect ratio 254: 242: 230: 201: 197:Hughes XF-11 178: 174:World War II 162: 152: 121: 119: 103:First flight 90:Number built 80:Primary user 61:Manufacturer 1637:(1960–1962) 1512:(1930–1962) 1187:Thunderbolt 546:Performance 538:Propellers: 524:Powerplant: 350:Long Island 245:trimetrogon 159:Development 149:World War 2 1805:Categories 1207:Thunderjet 1182:Thunderbug 649:References 596:Power/mass 471:Wing area: 145:jet engine 44:Strategic 843:0024-3019 654:Citations 459:Wingspan: 433:Data from 389:Plexiglas 265:propeller 249:Fairchild 126:prototype 114:June 1952 75:Cancelled 1084:Missiles 982:Fighters 931:Republic 605:See also 416:and the 373:Maryland 357:magazine 234:fuselage 1504:systems 1177:Swallow 1172:Snooper 1157:Rainbow 814:7 April 478:Airfoil 465:Height: 453:Length: 338:Pacific 282:ram air 270:nacelle 111:Retired 98:History 1779:RB-57F 1774:RB-57D 1733:RF-104 1728:RF-101 1455:AP-106 1450:AP-100 1167:Seabee 1162:Rocket 1147:Lancer 1060:RF-84F 1044:AP-100 1034:XF-103 1024:XF-84H 867:  841:  571:Range: 409:Pan Am 219:Design 72:Status 1786:RB-66 1769:RB-57 1764:RB-52 1759:RB-47 1754:RB-29 1749:RB-17 1723:RF-80 1672:SR-72 1667:SR-71 1649:RS-71 1644:RS-70 1445:AP-96 1440:AP-95 1435:AP-90 1425:AP-76 1420:AP-75 1415:AP-71 1410:AP-63 1405:AP-60 1400:AP-57 1395:AP-55 1390:AP-54 1385:NP-52 1380:NP-50 1375:NP-49 1370:NP-48 1365:AP-47 1360:AP-46 1355:AP-44 1350:AP-43 1345:AP-42 1340:AP-41 1335:AP-38 1330:AP-31 1325:AP-24 1313:AP-23 1308:AP-22 1303:AP-21 1298:AP-19 1293:AP-18 1288:AP-16 1283:AP-12 1278:AP-10 1140:Names 1075:XF-12 1039:F-105 1029:XF-91 1019:F-84F 1009:XP-72 1004:XP-69 966:XP-41 946:SEV-3 880:Wings 852:Wings 490:Root: 447:Crew: 324:XR-12 1718:RF-8 1713:RF-4 1622:R-16 1617:R-12 1612:R-11 1596:F-15 1591:F-14 1586:F-13 1581:F-12 1576:F-11 1571:F-10 1273:AP-9 1268:AP-8 1263:AP-7 1258:AP-6 1253:AP-5 1248:AP-4 1243:AP-3 1238:AP-2 1233:AP-1 1152:Loon 1127:RC-3 1122:RC-2 1117:RC-1 1091:JB-2 1070:SD-4 1065:SD-3 1014:F-84 999:P-47 994:P-44 989:P-43 961:A8V1 956:P-35 951:BT-8 865:ISBN 839:ISSN 835:Life 816:2021 526:4 × 496:Tip: 407:and 385:RC-2 379:RC-2 355:Life 261:cowl 207:and 153:RC-2 120:The 41:Type 1690:R-1 1566:F-9 1561:F-8 1556:F-7 1551:F-6 1546:F-5 1541:F-4 1536:F-3 1531:F-2 1526:F-1 1318:M/X 1101:KUW 1096:KGW 348:on 1807:: 1430:85 891:. 807:. 795:^ 692:^ 662:^ 375:. 371:, 326:. 309:. 297:. 236:. 1489:e 1482:t 1475:v 923:e 916:t 909:v 873:. 845:. 818:. 598:: 480:: 449:7 93:2

Index


aerial reconnaissance
Manufacturer
Republic Aviation
United States Army Air Forces
prototype
reconnaissance aircraft
Republic Aviation
radial engines
Pratt & Whitney R-4360 Wasp Major
jet engine
World War 2
United States Army Air Corps
Japanese homeland
World War II
Franklin D. Roosevelt
Elliot Roosevelt
Lockheed F-5 (a modified P-38 Lightning)
photo interpretation
Hughes XF-11
Boeing B-29 Superfortress
Boeing B-50 Superfortress
Boeing RB-47 Stratojet

fuselage
Aviation Week
trimetrogon
Fairchild
aspect ratio
cowl

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