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	Fact Sheets : Boeing B-56A : Boeing B-56A
		The B-47C was the initial designation for a design project initiated in January 1950 to redesign the aircraft for four Allison J35-A-23 turbojets in place of the six General Electric J47s.
		The original Allison J35-A-23s turbojets had estimated performance of 9,700 pounds thrust each at maximum power (with afterburners) and a normal power rating of 8,200 pounds thrust each.
		The actual J35 performance was no where near the estimates (about 7,400 pounds maximum power and 5,600 pounds normal) so alternative engines were proposed.
	www.nationalmuseum.af.mil /factsheets/factsheet.asp?id=2676 (494 words)

	Allison J35 - Wikipedia, the free encyclopedia
		The Allison J35 was originally developed by the General Electric Company in parallel with the Whittle-based centrifugal-flow J33, and was the Air Force's first axial-flow (straight-through airflow) compressor engine.
		The J35 was fairly simple, consisting of an eleven-stage axial-flow compressor and a single-stage turbine.
		The J35 was used to power the X-5 variable-sweep research aircraft and various prototypes such as the XB-43, XB-45, XB-46, XB-47, XB-48, and XB-49.
	en.wikipedia.org /wiki/Allison_J35 (182 words)

	Northrop YB-49
		Allison J35-A-5 turbojets buried inside the wing, four on each side.
		Allison J35-A-5 turbojets were mounted in banks of four on either side of the wing.
		The J35 turbojets of the YB-49 were extremely thirsty for fuel, and the jet-powered YB-49 had only half the range of the YB-35 that preceded it.
	home.att.net /~jbaugher2/b49_1.html (1569 words)

	Allison Engine Company - Wikipedia, the free encyclopedia
		The Allison Engine Company was a U.S. aircraft engine manufacturer which was acquired by Rolls-Royce plc in 1995 to become a subsidiary, Rolls-Royce Corporation.
		It was this reason in particular that the V-1710 was later removed from the P-51 Mustang and replaced with the Rolls-Royce Merlin instead.
		Over the years a family of engines, based on the T56 basic configuration has been developed, culminating in the T406/Allison AE1107 turboshaft for the V-22 Osprey, the Allison AE2100 turboprop, used on newer models of the C-130 and the Allison/Rolls-Royce AE 3007 turbofan which propels many commuter aircraft, such as the Embraer ERJ 135 family.
	en.wikipedia.org /wiki/Allison_Engine_Company (1004 words)

	Chanute Air Museum
		The J35 was the U.S. Air Force's first axial-flow compressor engine.
		It was first developed by General Electric, but in 1947 production responsibility for the engine was given to the Allison Division of General Motors.
		The J35 had an eleven-stage axial flow compressor and a single-stage axial turbine.
	www.aeromuseum.org /engines_j35.html (126 words)

	Welcome to AvWings
		The aircraft was to be powered by a pair of Allison J35 afterburning turbojets, mounted one on either side of the belly of the fuselage just underneath the wings.
		The engine air intakes were redesigned to include external boundary layer bleed ramps and auxiliary pop-in doors were added to the nacelle sides to allow additional air to be supplied to the engine during ground runups.
		After a rash of engine failures on early F-89Bs, the aircraft were reengined with Allison J35-A-21A turbojets, rated at 5100 lb.st.dry and 6800 lb.st with afterburning.
	www.avwings.com /pics/f89.html (3117 words)

	Allison
		Allison V-1710-27 thru 115 Overhaul Manual (part# 02-5AB-3)
		Allison V-1710-143, -145 1949 Parts Catalog (part# 02A-5AH-4)
		Allison V-1710-143, -145 1947 Overhaul Instructions (part# 02A-5AH-3)
	www.esscoaircraft.com /category_s/6515.htm (295 words)

	The Allison J35 turbojet = the fascinating story of the GE / Allison J35, the first USAF Axial Flow jet
		Like the Allison J33 centrifugal jet engine, the Allison J35 was based on a General Electric Design.
		A later development of the Allison J35 was produced as the Allison J71, which produced around 10,000lb thrust, which powered powered the Douglas B-66 "Destroyer" and the McDonnell F3H-2 "Demon".
		Allison J33 turbojet Allison J35 turbojet BMW 003 turbojet De Havilland Goblin turbojet General Electric J31 Jumo 004 turbojet Olympus593 MK610 Rolls Royce Avon turbojet
	www.wingweb.co.uk /engines/Allison_J35_turbojet.html (1130 words)

	[1.0] F-86A Through F-86D
		Some sources claim the J35 was a US copy of the de Havilland Goblin centrifugal-flow engine, but in fact the J35 an indigenous American axial-flow design, though it did leverage off British technology.
		The major difference was a longer and slenderer fuselage, partly achieved through the elimination of the structure and gear needed for carrier deck operation.
		Even with the J35 engine, the aircraft's speed was extremely impressive, roughly 150 KPH (93 MPH) faster than any other operational USAF fighter.
	www.faqs.org /docs/air/avf861.html (6126 words)

	The Boeing B
		With the speed and maneuverability of the fighters of the late forties, Boeing's swept-wing XB-47 won the bomber competition and swiftly transformed the XB-46 and the XB-48 into aviation footnotes.
		Six Allison J35-2 turbojet engines slung in pods beneath the swept-back wings gave the prototype Stratojet nimble performance, and helped to validate a design concept still widely used today.
		Although uprated J47-GE-3s were soon substituted, the B-47 also carried mountings for 18 solid-fuel booster rockets in the aft fuselage to shorten the takeoff roll.
	www.strategic-air-command.com /aircraft/B-47/b47-history.htm (1492 words)

	F - Fighter Aircraft
		1 General Electric J33-GE-11 or 1 Allison J33-A-9/17/25
		1 General Electric J33-GE-11 or 1 Allison J33-A-9/17/23/25
		1 Allison J35-A-25 or 1 Wright J65-W-1 Sapphire
	www.personal.psu.edu /users/d/o/dob104/aviation/us/fighter.html (189 words)

	Flying Wing
		With the end of WW II, and orders being placed for the competing Convair B-36 the fate of the piston engine B-35 was sealed, but Northrop, having forseen this possibility, received approval from the USAF to modify two of the YB-35's to jet power with the redesignation of YB-49.
		The second of these aircraft was powered by six 5,600 lb thrust Allison engines, four buried in the wings, and two in underslung pods.
		Air force officers gave very complimentary reports on the YB-49, and the service was convinced of the advantages of an all-wing aircraft, but in June of 1948, the second YB-49 was destroyed with the loss of its five man crew, which was attributed to structural failure.
	www.farmboyzimsflightsims.com /flyingwing.html (605 words)

	U.S jet fighter F-84 Republic Thunderstreak
		By August 1957, Republic and General Motors had built 1,410 F-84 's for TAC and SAC (USAF) and 1,301 for various NATO forces.The US Thunderstreaks were relegated to units of the ANG in the early 1960s.
		The YP-84A was powered by13 Allison engine instead of the General Electric power plant, had tiptanks and was armed with six.50in machine guns, four mounted in the nose and two in the wings.
		The basic design of the F-84 was completed before the end of that year after a long series of experiments and plans using various power plants which were being developed at that time.
	www.fiddlersgreen.net /AC/aircraft/Republic-F84/info/info.htm (1981 words)

	F-84 - The real meaning from Timesharetalk wikipedia (Site not responding. Last check: 2007-11-04)
		This was primarily due to severe shortage of spares for the Allison engines.
		Although the F-84B and F-84C could not be deployed because their J35 engines had a service life of only 40 hours, the F-84D and F-84E entered combat with 27th Fighter Escort Group on 7 December 1950.
		Two F-84Fs were converted into experimental aircraft with an Allison XT40-A-1 turboprop engine of 5,850 shaft horsepower (4,365 kW) driving a supersonic propeller.
	www.timesharetalk.co.uk /wiki.asp?k=F-84 (3727 words)

	Fact Sheets : Allison J35-A-35A Turbojet : Allison J35-A-35A Turbojet
		Originally developed by the General Electric Co., the J35 was the USAF's first axial-flow (straight-through airflow) compressor engine.
		Late in 1947 complete responsibility for the production of the engine was transferred to the Allison Division of General Motors.
		The J35 was used to power the X-5 variable-sweep research aircraft and various prototypes such as the XB-43, XB-45, XB-46, XB-47, XB-48 and XB-49.
	www.nationalmuseum.af.mil /factsheets/factsheet.asp?id=870 (174 words)

	Allison J35
		Developed by General Electric in parallel with the Whittle-based J33, the J35 was the U.S. Air Forces first axial-flow compressor turbojet.
		The J35 first flew in the XP-84 in 1946.
		Like the J33, responsibility for developing the J35 was transferred to Allison in 1946.
	www.shanaberger.com /engines/J35.htm (57 words)

	Revell’s 1/48th scale F-89C Scorpion
		Beginning with Block -25 aircraft, the engine was changed once again to the Allison J35-A-33A, creating 5,600 lbs thrust.
		The Allison J35-A-33A engine not only had more power, it also featured a redesigned inlet, de-icing equipment, inlet guide vanes, and redesigned forward engine mounts.
		Although the F-89C had made its maiden flight 18 September 1`951, the engine and wing failures kept the Scorpion from reaching its intended force levels until 1954.
	www.aircraftresourcecenter.com /Kits/RoG/1.48/F-89C/F-89C.htm (1157 words)

	DOUGLAS F-6A SKYRAY (FORMERLY F-4D-1)
		The Skyray was a carrier-based interceptor and strike fighter aircraft that was flown operationally by both the United States Navy and the Marine Corps.
		The first flight of the prototype powered by an Allison J35-A-17 turbojet engine was on 21 January 1951.
		Patuxent River test teams, working with Douglas Aircraft personnel, started evaluating their two prototype aircraft in mid-1952, with carrier suitability trials onboard USS CORAL SEA (CVA-43) in October 1953, and follow-on testing in 1954.
	www.paxmuseum.com /f4d/a6a.htm (266 words)

	Muche's Warbirds: The F-86 Sabre
		A variation of this design was offered to the Army Air Force which placed an order in late 1944 for one static test and two flying prototype aircraft to be designated as XP-86.
		Like the Fury, the XP-86 was to have straight wings and "straight through" jet flow for an Allison TG-180 (J35) turbojet engine.
		Allison J35-C-3 turbojet engine and in 1948 aircraft number one, AF s/n 45-59597, exceeded Mach 1, being the first U. fighter to officially do so.
	www.mucheswarbirds.com /F86art.html (1660 words)

	f7u-3
		These engines were later exchanged for Westinghouse J-46 engines with afterburner.
		The planned powerplant, two Westinghouse J46-WE-8 engines with 6000 pounds thrust and afterburners, was not available for the first 16 airplanes.
		These first 16 airplanes were powered by two Allison J35-A-29 engines.
	www.vought.com /heritage/products/html/f7u-3.html (338 words)

	NASA Dryden D-558-1 Skystreak Photo Collection
		The Skystreaks were turbojet powered aircraft that took off from the ground under their own power and had straight wings and tails.
		All three D-558-1 Skystreaks were powered by Allison J35-A-11 turbojet engines producing 5,000 pounds of thrust.
		All the Skystreaks were initially painted scarlet, which lead to the nickname "crimson test tube." NACA later had the color of the Skystreaks changed to white to improve optical tracking and photography.
	www1.dfrc.nasa.gov /gallery/photo/D-558-1 (380 words)

	The Beginner's Guide to the B-49
		The B-35 carried a crew of nine plus a relief crew of six.
		On the 1st of June, 1945, a contract was issued to Northrop for a jet engined version to be powered by eight Allison J35-A-5 engines of 4,000 pounds thrust.
		The six 5,000 pound thrust Allison J35-A-19 engines improved the speed and service ceiling.
	www.geocities.com /qcsms/articles/flying_wing.html (2559 words)

	Northrup F-89 Scorpion - Message Board - ezboard.com
		Since the XF-89 was somewhat underpowered and had poor takeoff characteristics, more powerful engines were fitted, Allison J35-A-21s, rated at 5200 lbst dry and 6800 lbst with afterburners.
		After a rash of engine failures on early F-89As, these aircraft were re-engined with Allison J35-A-21A turbojets, rated at 5100 lbst dry and 6800 lbst with afterburning.
		After a rash of engine failures on early F-89Bs, the aircraft were re-engined with Allison J35-A-21A turbojets, rated at 5100 lbst dry and 6800 lbst with afterburning.
	p090.ezboard.com /fjpspanzersfrm25.showMessage?topicID=151.topic (6263 words)

	Northrop F-89 Scorpion (Site not responding. Last check: 2007-11-04)
		Lockheed submitted a modified version of the T-33 model aircraft to be pro- duced as the F-94A.
		Northrop submitted a proposal labeled N-24, a slim-bodied model aircraft with a canti- levered mid-mounted wing and two Allison J35 turbojet engines with afterburners.
		The model aircraft was to have radar and a crew of two, with six 20 mm cannon in a unique trainable nose turret.
	www.aviationtrivia.homestead.com /F89.html (1223 words)

	North American F-86 Sabre - Message Board - ezboard.com
		The prototype flew in late 1946; it was an ugly aircraft, a stubby fat cigar with straight wings and an air intake in the nose, carrying six.50 cal machineguns, three on each side of the nose, and powered by a General Electric J35-GE-2 turbojet.
		The first production FJ-1 Fury was delivered in early 1948 with an Allison J35; the aircraft was clearly obsolescent even as it was being delivered, and the production was cut to a total of 30 fighters.
		One naval squadron was equipped with the Fury for about a year; the only distinction the type would attain is that it was the first operational jet fighter at sea.
	p090.ezboard.com /fjpspanzersfrm25.showMessage?topicID=92.topic (4144 words)

	North American F-86 (Site not responding. Last check: 2007-11-04)
		After scale model wind tunnel tests, the designers selected a wing that was swept back at an angle of 35 degrees, and added automatic leading edge slats to solve the stability problem.
		he first XP-86 flew on October 1, 1947, powered by an Allison J35-C-3, a 3,750 lb.
		In April 1948, the XP-86 exceeded Mach 1 (the speed of sound) in a shallow dive.
	www.nasm.si.edu /research/aero/aircraft/NAF-86.htm (595 words)

	AEREI X: le più importanti tappe della tecnologia aerospaziale USA
		L'aeroplano tedesco fu utilizzato presso le officine della Bell di Buffalo quale simulacro ingegneristico; il suo originale turboreattore Jumo 004B è stato sostituito con un Allison J35.
		Il NACA, continuando (come nel caso dell'X-2) ricerche di Busemann e Jones, era interessato ad un aereo con ali a freccia variabile in volo e valutò l'ipotesi di un X-1 o X-2 con questa caratteristica.
		Impianto propulsivo: un turboreattore Allison J35-A-17A da 2.225 kg/s al decollo.
	www.aereisuperfile.it /dossierX5.php (419 words)

	F-86 Sabre
		Sabre pilots enjoyed a 360 degree view of the surrounding skies, the fire power of six M-3.50 cal. machine guns and found the plane to be smooth and agile.
		Fitted at first with an Allison J35-A-5 turbojet, Sabre test pilots began to take the F-86A into the relatively unknown region of transonic speeds once it had the more powerful J-47 turbojet installed.
		The Sabre first "officially" broke the sound barrier in April 1948.
	www.cavanaughflightmuseum.com /Aircraft/F-86/Page1.html (524 words)

	X-5 index: X-5 Photo Gallery Contact Sheet
		The X-5 was a single-seat aircraft powered by an Allison J35-A-17A jet engine.
		It was 33.33 feet long with a wingspan of 20.9 feet (with the wings swept back at an angle of 60 degrees) to 33.5 feet (with the wings unswept).
		When fully fueled, the X-5 weighed 9,875 pounds.
	www.dfrc.nasa.gov /gallery/photo/X-5/HTML/index.html (433 words)

	Aircraft: Republic F-84C Thunderjet
		Production of the "C" model began in May of 1948.
		Features of the "C" model are its tri-cycle landing gear, wing tip fuel tanks, 6 x.50 Cal. machine guns, and the Allison J-35 turbojet rated at 4,000 Lbs.
		The ribbed canopy was retrofitted as an in-service modification; photos of F-84Cs, as built, indicate that early F-84s had clear canopies.
	www.marchfield.org /f84c.htm (430 words)

	Republic F-84 Thunderjet / F-84F Thunderstreak
		On 1944-09-11, the United States Army Air Forces released General Operational Requirements for a day fighter with a top speed of 600 mph (521 knots, 966 km/h), combat radius of 705 miles (612 nm, 1,135 km), and armament of either six 0.50 inch (12.7 mm) or four 0.60 inch (15.2 mm) machine guns.
		In addition, the new aircraft had to use the General Electric TG-180 axial turbojet which entered production as Allison J35.
		On 1944-11-11, Republic received an order for three prototypes of the new XP-84.
	www.fighter-planes.com /info/f84.htm (1738 words)

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