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Heinkel He 162 Volksjäger

From Wikipedia, the free encyclopedia
Interceptor jet aircraft, German, WW2
"Volksjäger" redirects here. For the Focke-Wulf project, seeFocke-Wulf Volksjäger.

He 162
He 162A, WkNr. 120230, during post-war trials in the USA
General information
TypeJet fighter
National originGermany
ManufacturerHeinkel
Primary userLuftwaffe
Number built120
History
Manufactured1945
Introduction dateJanuary 1945
First flight6 December 1944
RetiredMay 1945

TheHeinkel He 162Volksjäger (German, "People's Fighter") is a German single-engine, jet-poweredfighter aircraft fielded by theLuftwaffe late inWorld War II. Developed under theEmergency Fighter Program, it was designed and built quickly and made primarily of wood as metals were in very short supply and prioritised for other aircraft.Volksjäger was theReich Air Ministry's official name for the government design program competition won by the He 162 design. Other names given to the plane includeSalamander, which was the codename of its wing-construction program, andSpatz ("Sparrow"), which was the name given to the plane by theHeinkel aviation firm.[1]

The aircraft was notable for its small size.[a] It had a distinctive top-mounted engine which, combined with the aircraft's lowlanding gear, allowed the engine to be easily accessed for maintenance. This madebailing out of the aircraft without hitting the engine difficult, and the He 162 was the first single-engine aircraft provided with anejection seat in an operational setting. The small size left little room for fuel, which combined with the inefficient engine resulted in very low endurance - in the order of 20 minutes - and it only had room for twoautocannon, making it relatively underarmed for the era.

A series of fatal accidents during testing required a series of refinements that delayed the program. Although production lines were set up and deliveries began in early 1945, the impending defeat of Germany by that time made the effort pointless. Of nearly 1,000 aircraft on the assembly lines, only about 120 were delivered to the airfields and most of those never flew, usually due to shortages of parts, fuel, and pilots. Small numbers were used in development squadrons and these ultimately saw combat in a few cases during April 1945, yet the He 162 also proved to be quite dangerous to its own pilots as its tiny fuel load led to a number of aircraft crashing off field, while additional losses were attributed to structural failure.

Production was still running when thewar ended in May 1945. Numerous aircraft were captured by the Allied forces along with ample supplies of parts from the production lines.Eric Brown flew one just after the war and considered it a first-rate aircraft, albeit not suited for novice pilots. Several He 162s have been preserved in museum collections around the world.

Development

[edit]

State of the Luftwaffe fighter arm

[edit]

Through 1943, the U.S.Eighth Air Force (8AF) and GermanLuftwaffe entered a period of rapid evolution as both forces attempted to gain an advantage. Having lost too many fighters to the bombers' defensive guns, the Germans invested in a series of heavy weapons that allowed them to attack from outside the American machine guns' effective range. The addition of the 30 mm (1.2 in)MK 108, and even heavierBordkanone autoloading weapons in37 mm (1.5 in) and50 mm (2.0 in) calibres on theirZerstörer heavy fighters, and the adoption in spring 1943 of theWerfer-Granate 21 unguided rockets, gave the German single and twin-engined defensive fighters a degree of firepower never seen previously by Allied fliers. Meanwhile, single-engine aircraft likespecially equipped Fw 190As added armor to protect their pilots from Allied bombers' defensive fire, allowing them to approach to distances where their heavy weapons could be used with some chance of hitting the bombers. All of this added greatly to the weight being carried by both the single and twin-engine fighters, seriously affecting their performance.[2][3]

In early 1944, the 8AF re-opened its bombing campaign with theBig Week offensive in conjunction with the RAF, to force a decisive battle with Luftwaffe by attacking German aircraft production and so achieve Allied air superiority over Europe. The bombers returned to the skies with the long-rangeNorth American P-51 Mustang escort fighters progressively replacingRepublic P-47 Thunderbolts andLockheed P-38 Lightnings. Unencumbered with the heavy weapons needed to down a bomber, the Mustangs (and longer-ranged versions of other aircraft) were able to fend off theLuftwaffe with relative ease. TheLuftwaffe responded by changing tactics, forming in front of the bombers and making a single pass through the formations, giving the defense little time to react. Major GeneralJimmy Doolittle, commander of 8AF, had changed policy in January 1944; rather than forcing escorts to stay with the bomber formations, they were free to fly ahead of the bomber formations and roam freely over Germany to attack the Luftwaffe's defensive fighters wherever they could be found.[4]

This change in tactics resulted in a sudden increase in the rate of irreplaceable losses to the Luftwaffe day fighter force, as their heavily laden aircraft were "bounced" long before reaching the bombers.[5] Within weeks, many of their aces were dead, along with hundreds of other pilots, and the training program could not replace their casualties quickly enough. The Luftwaffe were able to put up little fight during the summer of 1944, allowing theAllied landings in France to go almost unopposed from the air. With few planes coming up to fight, Allied fighters were let loose on the German airbases, railways and truck traffic. Logistics soon became a serious problem for the Luftwaffe, as maintaining aircraft in fighting condition became almost impossible. Getting enough fuel was even more difficult because of a devastatingcampaign against German petroleum industry targets.[6][7]

Origins

[edit]
He 162120077, surrendered to the British at Leck, pictured at Freeman Field, Indiana, 1945

Addressing this posed a considerable problem for the Luftwaffe. Two camps quickly developed, both demanding the immediate introduction of large numbers of jet fighter aircraft. One group, led by GeneralAdolf Galland, theInspector of Fighters, reasoned that superior numbers had to be countered with superior technology, and demanded that all possible effort be put into increasing the production of the jet poweredMesserschmitt Me 262 in its A-1a fighter version, even if that meant reducing production of other aircraft in the meantime.[8]

The second group pointed out that this would likely do little to address the problem; the Me 262 had notoriously unreliableJumo 004 jet engines andlanding gear, and the existing logistics problems would mean there would merely be more of them on the ground waiting for parts that would never arrive, or for fuel that was not available.[9] Instead, they suggested that a new design be built – one so inexpensive that if a machine was damaged or worn out, it could simply be discarded and replaced with a fresh plane straight off the assembly line.[10] Thus was born the concept of the "throwaway fighter".[citation needed]

Galland and several other Luftwaffe senior officers expressed their vehement opposition to thislight fighter concept,[8][11] while head of the LuftwaffeReichsmarschallHermann Göring and Armaments MinisterAlbert Speer fully supported the idea. Göring and Speer got their way; accordingly, a contracttender to supply a single-engine jet fighter that was suited for cheap and rapid mass production was established under the nameVolksjäger ("People's Fighter").

Volksjäger

[edit]
See also:Emergency Fighter Program

The official RLMVolksjäger design competition parameters specified a single-seat fighter, powered by a singleBMW 003 turbojet,[12][13] a slightly lower-thrust engine not in demand for either the Me 262 or theArado Ar 234 jet bomber, already in service.[14] The main structure of theVolksjäger competing airframe designs would use cheap and unsophisticated parts made of wood and other non-strategic materials and, more importantly, could be assembled by semi- and non-skilled labor, includingslave labor.[15][16]

The specification stipulated various performance requirements, including a maximum weight of 2,000 kg (4,400 lb),[12] a maximum speed of 750 km/h (470 mph) at sea level, an operational endurance of at least a half hour, while the takeoff distance was to be no greater than 500 m (1,640 ft).[14] Provisions for armour plating in areas such as the fuel tanks and around the pilot were also to be made, however, manufacturers were also asked to provide detail on the aircraft's performance both with and without armour installed. The armament was specified as either a pair of 20 mm (0.79 in)MG 151/20 cannon with 100 rounds each, or two 30 mm MK 108 cannon with 50 rounds each.[17]

Furthermore, theVolksjäger needed to be easy to fly.[10] Some officials, such asArtur Axmann andKarl Saur, suggested even glider or student pilots should be able to fly the jet effectively in combat and, had theVolksjäger achieved widespread use, this would have been a likely occurrence.[18] After the war,Ernst Heinkel said, "[The] unrealistic notion that this plane should be a 'people's fighter,' in which theHitler Youth, after a short training regimen with clipped-wing two-seater gliders like theDFSStummel-Habicht, could fly for the defense of Germany, displayed the unbalanced fanaticism of those days."[19][20] The clipped-wingspan DFS Habicht models had varying wingspans of both 8 m (26 ft 3 in) or 6 m (19 ft 8 in), and were used to prepare more experiencedLuftwaffe pilots for the dangerousMe 163BKomet rocket fighter – the same sort of training approach would also be used for the Hitler Youth aviators chosen to fly theVolksjäger.[21]

On 8 September 1944, the requirement was issued to industry;[15][22] bidders were required to submit their basic designs within ten days while quantity production of the aircraft was to commence by 1 January 1945.[23] Because the winner of the new lightweight fighter design competition would be building huge numbers of the planes, nearly every German aircraft manufacturer expressed interest in the project, such asBlohm & Voss, andFocke-Wulf, whoseFocke-Wulf Volksjäger 1 design contender, likewise meant for BMW 003 turbojet power bore a resemblance to their slightly laterTa 183Huckebein jet fighter design. However, Heinkel had already been working on a series of "paper projects" for light twin-engine fighters over the last year under the designationP.1073, with most design work being completed by Professor Benz, and had gone so far as to build and test several models and conduct somewind tunnel testing.[24]

As Heinkel had a head start on its design, some officials believed that the outcome was a largely foregone conclusion.[17] Nevertheless, many companies opted to produce responses; some of these competing designs were technically superior (in particular to theBlohm & Voss P 211 proposal). Messerschmitt did not submit any design, the company's founder,Willy Messerschmitt, dismissed theVolksjäger concept to be a delusional failure.[25] During October 1944, the competition's results were announced, only three weeks following the requirement being issued; to little surprise, Heinkel's submission was selected for production.[26] In order to confuse Allied intelligence, the RLM chose to reuse the 8-162 airframe designation (formerly that of aMesserschmitt Bf 162 fast bomber);[27] Heinkel had reportedly requested another designation,He 500, for the aircraft.[28][29]

Design

[edit]
He 162 tail section

Heinkel had carried out some design work of a new twin-engine fighter with one engine placed on top of the aircraft and another under the nose, the highest point on the bottom of the fuselage. For the single-engine development, he removed the lower engine and repositioned the remaining upper engine just aft of thecockpit and centered directly over the wing's center section.[30] This arrangement simplified the overall balance of the aircraft, while also placing the engine in a convenient point for removal as it could be removed upward with a small crane.[31] The need for a crane to be present at every airfield that the aircraft would operate from was a point of contention of the aircraft from Heinkel's rivals.[32]

One consequence of the aircraft's basic configuration was that the jet exhaust would pass directly over the upper rear fuselage and the tail area. For this reason, the tail was constructed with two small vertical stabilizers positioned to either side of the exhaust's path, and the horizontal elevator mounted below it.[33] The horizontal section had considerabledihedral at 14º, raising the vertical stabilizers inline with the wing.[34]

The aircraft's relatively compact wing was mounted relatively high on the fuselage and was attached using four bolts.[12][33] The leading edge was straight while the trailing edge had a significant forward sweep. It was not possible to remove the wing without first removing the engine, an arrangement that would have hindered routine maintenance of the aircraft.[32] The combination of the engine being directly above the pilot and the wings on either side would make a conventional bailout very risky, so the aircraft was designed from the start to feature an ejection seat akin to the one used in theHeinkel He 219night fighter.[citation needed]

The main landing gear retracted into the fuselage below the wing and were of thetricycle layout.[33] Heinkel had significant previous experience with this layout on earlier designs including theHeinkel He 280,[35][36] however, this was the first of their designs to use this layout from the start. A small window in the lower cockpit between the rudder pedals allowed the pilot to visually check whether the gear was down.[37][38][39] Partly due to the late-war period it was designed within, some of the He 162's landing gear components were "recycled" existing landing gear components from a contemporary German military aircraft to save development time: the main landing gear's oleo struts and wheel/brake units came from theMesserschmitt Bf 109K, as well as the double-acting hydraulic cylinders, one per side, used to raise and lower each maingear leg.[40]

Prototypes

[edit]

The He 162 V1 first prototype flew within an astoundingly short period of time: the design was chosen on 25 September 1944 and first flew on 6 December,[31][41] less than 90 days later. This was despite the fact that the factory inWuppertal makingTego filmplywood glue — used in a substantial number of late-war German aviation designs whose airframes and/or major airframe components were meant to be constructed mostly from wood —had been bombed by the Royal Air Force and a replacement had to be quickly substituted, without realizing that the replacement adhesive was highly acidic and would disintegrate the wooden parts it was intended to be fastening.[42]

The first flight of the He 162 V1, byFlugkapitän Gotthold Peter – the first German jet fighter aircraft design to be jet-powered from its maiden flight onward – was fairly successful, but during a high-speed run at 840 km/h (520 mph), the highly acidic replacement glue attaching the nose gear strut door failed and the pilot was forced to land. Other problems were noted as well, notably a pitch instability and problems with sideslip due to therudder design.[12][43] None were considered important enough to hold up the production schedule for even a day. On a second flight on 10 December, again with Peter at the controls, in front of various Nazi officials, the glue again caused a structural failure. This allowed theaileron to separate from the wing, causing the plane to roll over, it broke up in the air and crashed, killing Peter.[31][44]

An investigation into the failure revealed that the wing structure had to be strengthened and some redesign was needed, as the glue bonding required for the wood parts was in many cases defective.[31][42] However, the schedule was so tight that testing was forced to continue with the current design. Speeds were limited to 500 km/h (310 mph) when the secondprototype flew on 22 December. This time, the stability problems proved to be more serious, and were found to be related to phenomenon known asDutch roll.[45]While this tendency could be resolved by reducing the dihedral, however, as the He 162 was supposed to enter production within weeks, there was no time to implement major design changes. Instead, a number of small changes were made, such as the addition oflead ballast in the nose to move thecentre of gravity towards the front of the aircraft while the tail surfaces were also slightly increased in size.[citation needed] Despite these measures, some figures, such asAlexander Lippisch, declared the flying characteristics of the He 162 to be unsuitable for inexperienced pilots.[46]

The third and fourth prototypes, which used an "M" for "Muster" (model) number instead of "V" for "Versuchs" (experimental) number, as the He 162 M3 and M4, after being fitted with the strengthened wings, flew in mid-January 1945.[47][48] These versions also included – as possibly the pioneering example of their use on a production-line, military jet aircraft – small, anhedraledaluminium"drooped" wingtips, reportedly designed by Alexander Lippisch and known in German asLippisch-Ohren ("Lippisch Ears"), in an attempt to cure the stability problems via effectively "decreasing" the main wing panels' marked three degree dihedral angle.[49] Both prototypes were equipped with two 30 mm (1.18 in) MK 108 cannon in the He 162 A-1 anti-bomber variant; in testing, the recoil from these guns proved to be too much for the lightweight fuselage to handle, and plans for production turned to the A-2 fighter with two 20 mm MG 151/20 cannon instead while a redesign for added strength started as the A-3. The shift to 20 mm guns was also undertaken because the smaller-calibre weapons would allow more ammunition to be carried.[citation needed]

The He 162 was originally built with the intention of being flown by the Hitler Youth, as the Luftwaffe was fast running out of pilots. However, the aircraft's complexity required more experienced pilots. Both a standard-fuselage length, unarmed BMW 003E-powered two-seat version (with the rear pilot's seat planned to have a ventral access hatch to access the cockpit) and an unpowered two-seatglider version, designated the He 162S (Schulen), were developed fortraining purposes.[50] Only a small number were built, and even fewer delivered to the sole He 162 Hitler Youth training unit to be activated (in March 1945) at an airbase atSagan. The unit was in the process of formation when the war ended, and did not begin any training; it is doubtful that more than one or two He 162S gliders ever took to the air.[citation needed]

TheHinterbrühl underground production line for the He 162A was captured in April 1945

Various changes had raised the weight over the original 2,000 kg (4,410 lb) limit, but even at 2,800 kg (6,170 lb), the He 162 was still among the fastest aircraft in the air with a maximum airspeed of 790 km/h (427 kn; 491 mph) at sea level and 839 km/h (453 kn; 521 mph) at 6,000 m (20,000 ft),[51] but could reach 890 km/h (481 kn; 553 mph) at sea level and 905 km/h (489 kn; 562 mph) at 6,000 m (20,000 ft) using short burst extra thrust.[52] The short flight duration of barely 30 minutes was due to only having a single 695-litre (183 US gallon) capacity flexible-bladder fuel tank in the fuselage directly under the engine's intake.[53] The originalBaubeschreibung document submittal for the He 162 dated mid-October 1944 showed a pair of fuel tanks for the original version of theSpatz's airframe as-designed: a single, smaller capacity 640 litre (169 US gal) fuselage main tank in approximately the same location as the later 695 litre tank was placed, with an additional wing centre-section tank just above and behind it, never produced for the production run, of some 325 litres (86 US gal) feeding by gravity into the main fuselage tank.[54] The A-2 version, in some examples (as the one flown byRoyal Navy test pilotCaptain Eric Brown postwar) had an emplacement of a pair of "impregnated" 180 litre (47.5 US gal) wing tanks, one built into each inner wing panel, within the first fourwing ribs out from the root and between the spars, that fed into the main 695 litre fuselage tank in a similar manner to what the earlier 325 litre center-section tank had been proposed to do; but were themselves ungauged, their exhaustion of fuel only marked when the main fuel gauge began to fall during flight.[55] The production He 162A-2 was armed with a pair of MG 151/20 cannon.[51][56]

Multiple facilities were engaged in the production of the He 162, including the assembly lines inSalzburg, theHinterbrühl, and theMittelwerk.[51][57] By April 1945, it had been anticipated that output would reach 1,000 aircraft per month, which was double the rate achieved when the Mittelwerk plant commenced deliveries.[51] Furthermore, the Air Ministry expected that production were rise even beyond this figure in order to produce sufficient fighter coverage.[58][59]

Operational history

[edit]

During January 1945, the Luftwaffe formed anErprobungskommando 162 ("Test Unit 162") evaluation group to which the first 46 aircraft were delivered. The group was based at the Luftwaffe main test center, orErprobungsstelle atRechlin.

In February, deliveries of the He 162 commenced to its first operational unit, I./JG 1 (1st Group ofJagdgeschwader 1Oesau — "1st Fighter Wing"), which had previously flown the Focke-Wulf Fw 190A. I./JG 1 was transferred toParchim, which, at the time, was also a base for the Me 262-equippedJagdgeschwader 7, some 80 km south-southwest of the Heinkel factory's coastal airfield at "Marienehe" (today known asRostock-Schmarl, northwest of the Rostock city centre), where the pilots could pick up their new jets and start intensive training beginning in March 1945. This was all happening simultaneously with unrelenting Allied air attacks on the transportation network, aircraft production facilities andpetroleum,oil, andlubrication (POL) product-making installations of the Third Reich – these had now begun to also target the Luftwaffe's jet and rocket fighter bases as well. On 6 April, theUSAAF bombed the field at Parchim with 134Boeing B-17 Flying Fortresses, inflicting serious losses and damage to the infrastructure.[60] Two days later, I./JG 1 moved to an airfield at nearbyLudwigslust and, less than a week later, moved again to an airfield atLeck, near the Danish border. On 8 April, II./JG 1 moved to Heinkel's aforementioned Rostock northwestern coastal suburban factory airfield and started converting from Fw 190As to He 162s. III./JG 1 was also scheduled to convert to the He 162, but theGruppe disbanded on 24 April and its personnel were used to fill in the vacancies in other units.[citation needed]

The He 162 first saw combat in mid-April 1945. On 19 April,Feldwebel Günther Kirchner shot down aRoyal Air Force fighter and, although the victory was credited to a flak unit, the British pilot confirmed during interrogation that he had been downed by an He 162.[61][62] The Heinkel and its pilot were both lost that same day as well, having been shot down over Husum[63] by Flying Officer Geoffrey Walkington,[64][65] piloting an RAFHawker Tempest. Though still in training, I./JG 1 began to score kills in mid-April, but went on to lose 13 He 162s and 10 pilots. Ten of the aircraft were operational losses, caused byflameouts and sporadic structural failures. Only two of the 13 aircraft were actually shot down. The He 162's 30-minute fuel capacity also caused problems, as at least two of JG 1's pilots were killed attempting emergencydeadstick landings after exhausting their fuel.[citation needed]

During its exceedingly brief operational service career, the He 162's cartridge-type ejector seat was employed under combat conditions by JG 1's pilots at least four times. Kirchner had been the first to eject when he was attacked on April 19, but he was too low and was killed when his parachute failed to open.[66][67] The second recorded use was by Lt Rudolf Schmidt on April 20, with Fw. Erwin Steeb ejecting from his He 162 the following day. Finally, Hptm.Paul-Heinrich Dähne attempted to eject from his aircraft on April 24, but was killed when the cockpit canopy failed to detach.[citation needed]

A captured He 162, circa 1945
Captured He 162120230 in France, brought to the US byOperation Lusty

In the last days of April, as the Soviet troops approached, II./JG 1 evacuated from Marienehe and on 2 May joined the I./JG 1 atLeck. On 3 May, all of JG 1's surviving He 162s were restructured into two groups, I.Einsatz ("Combat") and II.Sammel ("Collection"). All JG 1's aircraft were grounded on 5 May, whenGeneral AdmiralHans-Georg von Friedeburg signed the surrender of all German armed forces in the Netherlands, Northwest Germany and Denmark. On 6 May, when the British reached their airfields, JG 1 turned their He 162s over to the Allies.[68] Numerous aircraft were shipped to the U.S., Britain, France, and the Soviet Union for further evaluation.[69][70]

Erprobungskommando 162 fighters, which had been passed on toJV 44, an elite jet unit under Adolf Galland a few weeks earlier, were all destroyed by their crews to keep them from falling into Allied hands. Heinkel did not resort to such measures, the company's engineers supplied the Americans with detailed designs for the He 162.[71]

The difficulties experienced by the He 162 are believed to have been primarily a result of its rush into production, rather than any inherent design flaw.[72] One experiencedLuftwaffe pilot who flew the He 162 called it a "first-class combat aircraft."[citation needed]Test pilot Eric Brown of theFleet Air Arm, who flew a record 486 different types of aircraft, said the He 162 "was a superb aeroplane in its element, but quite a handful to take off and land. Never met better flying controls yet they could easily be so mishandled..." and "it was no aeroplane to let embryo pilots loose on".[73] Brown had been warned to treat the rudder with suspicion due to a number of in-flight failures. This warning was passed on by Brown to RAF pilotFlight Lieutenant R. A. Marks, but was apparently not heeded. On 9 November 1945, during a demonstration flight fromRAE Farnborough, one of the fin and rudder assemblies broke off at the start of a low-level roll causing the aircraft to crash into Oudenarde Barracks,Aldershot, killing Marks and a soldier on the ground.[74]

He 162Mistel

[edit]

TheMistel series of fighter/powered bomb compositeground-attack aircraft pre-dated the He 162 by over two years, and theMistel 5 project study in early 1945 proposed the mating of an He 162A-2 to theArado E.377A flying bomb.[31][75] The fighter would sit atop the bomb, which would itself be equipped with two underwing-mounted BMW 003 turbojets. This ungainly combination would take off on a sprung trolley fitted with tandem wheels on each side for the "main gear" equivalent, derived from that used on the first eight Arado Ar 234 prototypes, with all three jets running. Immediately after take-off, the trolley would be jettisoned, and theMistel would then fly to within strike range of the designated target. Upon reaching this point, the bomb would be aimed squarely at the target and then released, with the jet turning back for home. TheMistel 5 remained a "paper project", as the Arado bomb never progressed beyond the blueprint stage.[citation needed]

Variants

[edit]
  • He 162 A-0 — first ten pre-production aircraft.
  • He 162 A-1 — armed with two 30 mm (1.18 in) MK 108 cannons with 50 rounds per gun.
  • He 162 A-2 — armed with two 20 mm MG 151/20 cannons with 120 rounds per gun.
  • He 162 A-3 — proposed upgrade with reinforced nose mounting twin 30 mm MK 108 cannons.
  • He 162 A-8 — proposed upgrade with the more powerful Jumo 004D-4 engine of 10.3 kN (2,300 lbf) top thrust levels.Muster (model) prototype airframes M11 and M12's testing revealed a top speed of 885 km/h (550 mph) at sea level at normal thrust and 960 km/h (597 mph) with maximum thrust,[76] close to the Me 163B rocket fighter's top velocity figures.
  • He 162 B-1 — a proposed follow on planned for 1946, meant to use the Heinkel firm's own, more powerful 12 kN (2,700 lb) thrustHeinkel HeS 011A turbojet, a stretched fuselage to provide more fuel and endurance as well as increasedwingspan, with reduced dihedral which allowed the omission of theanhedral wingtip devices. To be armed with twin 30 mm (1.18 in) MK 108s.
The He 162B airframe was also used as the basis for theMiniature Fighter Project design competition powered by one or two "square-intake" Argus As 044pulsejet engines. The pulsejet, however didn't provide enough thrust for takeoff and neither Heinkel nor theOKL showed much enthusiasm for the project.[77]
  • He 162C — proposed upgrade featuring the B-series fuselage, Heinkel HeS 011A engine, swept-back, anhedraled outer wing panels forming agull wing, a newV-tail stabilizing surface assembly, and upward-aimed twin 30 mm (1.18 in) MK 108s as aSchräge Musik weapons fitment,[citation needed] located right behind the cockpit.
  • He 162D — proposed upgrade with a configuration similar to C-series but a dihedraledforward-swept wing.[62][78]
  • He 162E — He 162A fitted with the BMW 003R mixed power plant, a BMW 003A turbojet with an integratedBMW 718 liquid-fuel rocket engine — mounted just above the exhaust orifice of the turbojet — for boost power. At least one prototype was built and flight-tested for a short time.
  • He 162S — two-seat training glider.

Operators

[edit]
Nazi Germany
France
United Kingdom

Aircraft on display

[edit]
  • Wk. Nr. 120235, Imperial Duxford)
    Wk. Nr. 120235, Imperial Duxford)
  • Wk. Nr. 120086, Canada Aviation and Space Museum, Ottawa
    Wk. Nr. 120086, Canada Aviation and Space Museum, Ottawa
Reproduction

Specifications (He 162A)

[edit]
He 162A 3-view

Data fromHitler's Luftwaffe.[53]

General characteristics

  • Crew: 1
  • Length: 9.05 m (29 ft 8 in)
  • Wingspan: 7.2 m (23 ft 7 in)
  • Height: 2.6 m (8 ft 6 in)
  • Wing area: 11.16 m2 (120.1 sq ft)
  • Empty weight: 1,660 kg (3,660 lb)
  • Max takeoff weight: 2,800 kg (6,173 lb)
  • Fuel capacity: 695 L (184 US gal; 153 imp gal)
  • Powerplant: 1 ×BMW 109-003E-1 orBMW 109-003E-2turbojet engine, 7.85 kN (1,760 lbf) thrust

Performance

  • Maximum speed: 840 km/h (520 mph, 450 kn) at 6,000 m (20,000 ft)[b]
  • Range: 975 km (606 mi, 526 nmi)
  • Service ceiling: 12,000 m (39,000 ft)
  • Rate of climb: 23.42 m/s (4,610 ft/min)
  • Wing loading: 252 kg/m2 (52 lb/sq ft)
  • Thrust/weight: 0.35 (normal thrust)
0.41 (emergency boosted thrust)

Armament

See also

[edit]

Aircraft of comparable role, configuration, and era

Related lists

References

[edit]

Notes

[edit]
  1. ^Although almost the same length as aMesserschmitt Bf 109, itswingspan was much shorter at 7.2 metres (24 ft) vs. 9.9 metres (32 ft) for the Bf 109
  2. ^ 790 km/h (490 mph; 430 kn) atsea level normal thrust, 890 km/h (550 mph; 480 kn) at sea level emergency boosted thrust, and 905 km/h (562 mph; 489 kn) at 6,000 m (20,000 ft) emergency boosted thrust

Citations

[edit]
  1. ^"Heinkel He 162 A-2 Spatz (Sparrow)".airandspace.si.edu. Smithsonian Institution National Air & Space Museum. Retrieved25 September 2021.Pilots mastered some of the Spatz's nasty habits but the jet would always be a difficult, even dangerous, aircraft to fly, even for experienced pilots...the He 162 has often been erroneously referred to as the Salmander. The term is a codename for the wing structure, not the aircraft.
  2. ^Weal 1996, p. 78.
  3. ^Forsyth 2009, pp. 58–59.
  4. ^McFarland and Newton 1991, pp. 160–161.
  5. ^Hess 1994, pp. 77–78.
  6. ^Miller 2006, p. 320.
  7. ^Williamson, Charles C.; Hughes, R. D.; Cabell, C. P.; Nazarro, J. J.; Bender, F. P.; Crigglesworth, W. J. (5 March 1944). Plan for Completion of Combined Bomber Offensive.Dwight D.Eisenhower Presidential Library: Smith, Walter Bedell: Collection of World War II Documents, 1941–1945; Box No.: 48 (Report). HQ, U.S.S.T.A.F.
  8. ^abDorr 2013, p. 153.
  9. ^Forsyth 2016, p. 8.
  10. ^abForsyth 2016, p. 7.
  11. ^Uziel 2011, pp. 240–243.
  12. ^abcdChristopher 2013, p. 145.
  13. ^LePage 2009, p. 38.
  14. ^abForsyth 2016, pp. 8–9.
  15. ^abLePage 2009, p. 244.
  16. ^Dorr 2013, p. 152.
  17. ^abForsyth 2016, p. 10.
  18. ^Forsyth 2016, pp. 17–18.
  19. ^Excerpt from Lucas Arts' "Secret Weapons of Luftwaffe" CD-ROM's Text Manual.
  20. ^Heath 2022, p. 223.
  21. ^Forsyth 2016, pp. 7–8.
  22. ^Dorr 2013, p. 151.
  23. ^Forsyth 2016, p. 9.
  24. ^Forsyth 2016, pp. 9–10.
  25. ^Forsyth 2016, p. 11.
  26. ^Forsyth 2016, p. 15.
  27. ^Sharp 2020b, p. 16.
  28. ^Sharp 2020b, p. 178.
  29. ^Forsyth 2016, p. 22.
  30. ^Sharp 2020b, pp. 177–178.
  31. ^abcdeFord 2013, p. 224.
  32. ^abForsyth 2016, p. 14.
  33. ^abcDorr 2013, p. 150.
  34. ^"Baubeschreibung des einmotorigen Jagdeinsitzers, Baumuster 162, mit TL-Triebwerk BMW 003 E-1 (in German)"(PDF).deutsche-luftwaffe.de. Heinkel Flugzeugwerke. 15 October 1944. p. 40. Archived fromthe original(PDF) on 4 August 2016. Retrieved6 July 2016.
  35. ^Christopher 2013, p. 58.
  36. ^Sharp 2020b, p. 72.
  37. ^abHeinkel 162 (He162) landing gear test(YouTube) (YouTube). Le Bourget, Paris, France: memorialflight. 2008. Retrieved9 July 2013.
  38. ^Animation of He 162 nosegear retraction cycle
  39. ^Animation of He 162 maingear retraction cycle
  40. ^Sengfelder, Günther (1993).German Aircraft Landing Gear. Atglen, PA USA: Schiffer Publishing. pp. 136–137.ISBN 0-88740-470-7.
  41. ^Forsyth 2016, pp. 24–25.
  42. ^abDorr 2013, p. 156.
  43. ^Forsyth 2016, pp. 25–29.
  44. ^Sharp 2020b, p. 18.
  45. ^Sharp 2020b, p. 155.
  46. ^Sharp 2020b, p. 311.
  47. ^Sharp 2020b, p. 11.
  48. ^Forsyth 2016, pp. 30–32.
  49. ^"Baubeschreibung des einmotorigen Jagdeinsitzers, Baumuster 162, mit TL-Triebwerk BMW 003 E-1 (in German)"(PDF).deutsche-luftwaffe.de. Heinkel Flugzeugwerke. 15 October 1944. p. 39. Archived fromthe original(PDF) on 4 August 2016. Retrieved6 July 2016.
  50. ^Forsyth 2016, p. 51.
  51. ^abcdChristopher 2013, p. 146.
  52. ^Donald 1994, p. 119.
  53. ^abWood and Gunston 1977, pp. 194–195.
  54. ^"Baubeschreibung des einmotorigen Jagdeinsitzers, Baumuster 162, mit TL-Triebwerk BMW 003 E-1 (in German)"(PDF).deutsche-luftwaffe.de. Heinkel Flugzeugwerke. 15 October 1944. p. 43. Archived fromthe original(PDF) on 4 August 2016. Retrieved6 July 2016.
  55. ^Brown 2010, p. 137.
  56. ^Dorr 2013, p. 159.
  57. ^Dorr 2013, pp. 154–155.
  58. ^LePage 2009, p. 267.
  59. ^Sharp 2020b, p. 179.
  60. ^Forsyth 2016, p. 62.
  61. ^Mombeek 1992, p. 297.
  62. ^abDorr 2013, p. 160.
  63. ^"Victories".www.hawkertempest.se. Retrieved31 December 2023.
  64. ^Shores 2006, pp. 497–498.
  65. ^Thomas and Holmes 2016, pp. 60–61.
  66. ^Shores 2006, p. 498.
  67. ^Thomas and Holmes 2016, p. 60.
  68. ^Forsyth 2016, p. 81.
  69. ^Dorr 2013, p. 161.
  70. ^Forsyth 2016, pp. 6–7.
  71. ^Sharp 2020b, p. 148.
  72. ^LePage 2009, p. 266.
  73. ^Brown 2010, p. 138.
  74. ^"Two Killed In Flying Accident".The Times. London, England. 10 November 1945. p. 2.
  75. ^LePage 2009, pp. 160–161.
  76. ^"History and Experiences of He-162"(PDF).wwiiaircraftperformance.org. Retrieved11 August 2023.
  77. ^The Heinkel He-162 Volksjaeger
  78. ^Sharp 2020b, p. 20.
  79. ^abSimpson, Andrew (2015)."Individual History: Heinkel He162A-2 W/NR.120227/AIR MIN 65/VN679/8472M, Museum Accession Number 1990/0697/A"(PDF).Royal Air Force Museum. Retrieved30 November 2022.
  80. ^Forsyth & Creek 2008, p. 180
  81. ^"Heinkel He 162 A-2 Spatz (Sparrow)".Smithsonian Institution. Retrieved30 November 2022.
  82. ^"Heinkel He 162A-1 Volksjäger (120086)".ingeniumcanada.org. Canada Aviation and Space Museum. Retrieved5 February 2023.
  83. ^Sharp 2020a, p. 133
  84. ^"Medieninfo: Heinkel He 162". Deutsches Technikmuseum Berlin. Archived fromthe original on 29 May 2012. Retrieved26 November 2011.
  85. ^"Heinkel 162A-1 Salamander". Imperial War Museum. Retrieved30 November 2022.
  86. ^Forsyth & Creek 2008, p. 181

Bibliography

[edit]

Further reading

[edit]
  • Balous, Miroslav; Bílý, Miroslav (2004).Heinkel He 162 Spatz (Volksjäger) (in Czech and English). MBI.ISBN 80-86524-06-X.
  • Couderchon, Philippe (April 2006). "The Salamander in France Part 1".Aeroplane Magazine.
  • Couderchon, Philippe (May 2006). "The Salamander in France Part".Aeroplane Magazine.
  • Green, William (1970).Warplanes of the Third Reich. Macdonald and Jane's Publishers Ltd.ISBN 0-356-02382-6.
  • Griehl, Manfred (2007).The Luftwaffe Profile Series No.16: Heinkel He 162. Schiffer Publishing.ISBN 978-0-7643-1430-8.
  • Griehl, Manfred (2007).Heinkel Strahlflugzeug He 162 "Volksjäger" — Entwicklung, Produktion und Einsatz (in German). Stedinger Verlag.ISBN 978-3-927697-50-8.
  • Hiller, Alfred (1984).Heinkel He 162 "Volksjäger" — Entwicklung, Produktion, Einsatz. Verlag Alfred Hiller.
  • Ledwoch, Janusz (1998).He-162 Volksjager (Wydawnictwo Militaria 49). Wydawnictwo Militaria.ISBN 83-86209-68-2.
  • Müller, Peter (2006).Heinkel He 162 "Volksjäger": Letzter Versuch der Luftwaffe (in German and English). Müller History Facts.ISBN 3-9522968-0-5.
  • Myhra, David (1999).X Planes of the Third Reich: Heinkel He 162. Schiffer Publishing.ISBN 0-7643-0955-2.
  • Nowarra, Heinz J. (1993).Heinkel He 162 "Volksjager". Schiffer Publishing.ISBN 0-88740-478-2.
    • (Translation of:Der "Volksjäger" He 162 (in German). Podzun-Pallas Verlag. 1984.ISBN 3-7909-0216-0..)
  • Peter-Michel, Wolfgang (2011).Flugerfahrungen mit der Heinkel He 162;— Testpiloten berichten (in German). BOD-Verlag.ISBN 978-3-8423-7048-7.
  • Smith, J. Richard; Creek, Eddie J. (1986).Heinkel He 162 Volksjager. Monogram Close-Up. Vol. 11. Monogram Aviation Publications.ISBN 0-914144-11-1.
  • Smith, J. Richard; Kay, Anthony (1972).German Aircraft of the Second World War (Third (1978) ed.). Putnam & Company.ISBN 0-370-00024-2.

External links

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Heinkel aircraft
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