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Hafner Rotachute

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225: 200:. On 29 May 1942, the first flight of the Rotachute Mark II was achieved while under tow behind a Jeep, and several more towed flights were also successful. Meanwhile, the Mark III had been produced, with a tail section comprising a wooden framework covered in doped linen fabric plus a rigid tailplane. Starting on 2 June 1942, the Rotachute Mark III was flown at heights up to 100 ft (30.5 m) while under tow behind a Jeep, with tow rope lengths up to 300 ft (91.4 m). From 9 June, successful inflight releases and landings were achieved while under tow. 141:. In October 1940, work began on design and construction of rotor systems and scale models of rotor kites. The first models were made of wood and fabric, ballasted to represent a pilot, and had a rotor span of about 3 ft (0.91 m). They were tested successfully by hand launching, but suffered buffeting and lack of autorotation when launched from aircraft at height. The third evolution, designated "M.3", had metal rotor blades, and after further modifications made the first successful launch and descent from a 39: 158:
framework with a single seat, rubber-mounted rotor hub, hanging control column, skid undercarriage, and a self-inflating rear fairing made of rubberised fabric with integral tailplane. The two rotor blades, of wooden construction, could achieve flapping and coning characteristics via hinges on the rotor hub. Fixed footrests were provided, plus fittings below the seat to accommodate a soldier's weapon, such as a
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and a longer test flight at RAF Snaith were both more successful. The flexible tail section evidently offered inadequate directional stability, and the consequence was the Rotachute Mark II, that had a longer tail section braced with wooden formers, plus two landing wheels mounted below the centre of
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The design of the man-carrying machine known as a Rotachute, also known as a Hafner H.8, evolved from November 1940 and throughout 1941. In September 1941, the Central Landing Establishment was renamed the Airborne Forces Establishment. The Rotachute Mark I design initially comprised a tubular steel
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In January 1942, trials of the Rotachute Mark I were conducted to assess the aerodynamic characteristics while on the truck-mounted rig, with pilot control of the aircraft in forward motion. On 11 February 1942, the prototype Rotachute was first manually flown from a wheeled trolley while under tow
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The Rotachute was the eventual development of a concept devised by Raoul Hafner, an Austrian engineer who specialised in rotary wing design, and who had moved to the UK in 1933 to continue his research and development work. In 1940, he proposed the use of a single-place strap-on rotor kite in place
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Although the Rotachute concept had proved to be practical, the operational requirement for such a machine never materialised. About eight Rotachutes were constructed, most being progressively converted to Mark III and then to Mark IV specifications. They continued to be flown in ground-based and
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From 17 June 1942, a Rotachute Mark III was air-towed behind a Tiger Moth on a 300 ft (91.4 m) tow line. After two towed flights, the Rotachute was released at an altitude of 200 ft (61 m) and made the first manned free flight and controlled landing. Further free flights were made from
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No. 11/42 was issued retrospectively to describe the outline requirements. The Ministry of Aircraft Production sub-contracted construction of parts to specialist firms including F. Hills and Sons, Airwork General Trading, Dynaflex, Dunlop, and H. Morris & Co. Some full size rotor trials were
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of a conventional parachute, to deliver a soldier accurately to a battlefield. The proposal was made to the Air Ministry in the light of a shortage of silk for parachute manufacture. Hafner was briefly interned as an alien, but was released to pursue the feasibility of the idea at the
145:. Further developments and tests continued into February 1941. The tenth evolution scale model (M.10) had mass-balanced wooden rotors, ballast of 100 lb (45.3 kg), and a rotor span of 10 ft (3.05 m). On 14 March 1941, the M.10 model was successfully air-launched from a 184:. On that and on a subsequent trial, the machine rolled over after landing, sustaining damage to the blades but not to the pilot. A tethered test beneath a 196:(AFEE), still based at Ringway. The rotary wing section of AFEE continued to conduct tests on longer runways during detachments at RAF Snaith and 167:
carried out using a pivoting rig mounted on a Ford flatbed truck, and full-size unmanned airframes were used in ground-based and inflight trials.
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behind a Humber car at Ringway, after starting the rotor by hand. The pilot was Flt Lt I.M. Little, who had experience flying
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The fifth aircraft (P-5) was a Rotachute Mark III, converted in 1943 to the Mark IV configuration, and is displayed at the
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inflight trials until late 1943, to help research flight characteristics for a follow-on project, the
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altitudes up to 3,900 ft (1,189 m). On 1 July 1942, AFEE moved its main base from Ringway to
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On 15 February 1942, the unit was again reorganised, to form the
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autogiros on radar calibration duties; he was later awarded the
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Serge Van Heertum; Philippe Decock; Marc Arys (2015).
246: 459:Jarrett, Philip. "Nothing Ventured ... Part 17". 569: 46:Ground test of a Rotachute III at Ringway, 1942 494: 501: 487: 319:108 mph (173.8 km/h, 94 kn) 194:Airborne Forces Experimental Establishment 508: 377: 375: 373: 371: 369: 367: 365: 355: 353: 351: 349: 347: 345: 152: 116:was a British 1940s experimental one-man 223: 14: 570: 362: 342: 170: 482: 583:1940s British experimental aircraft 24: 474:Rotachute at Museum of Army Flying 393:"Middle Wallop Army Flying Museum" 304:177 sq ft (16.44 m) 298:15 ft 0 in (4.57 m) 274:10 ft 0 in (3.05 m) 25: 599: 467: 397:Sierra Bravo Aero Pictures (SBAP) 280:5 ft 0 in (1.52 m) 247:Specifications (Rotachute Mk III) 37: 463:, August 1991, pp. 470–476 439: 410: 384: 13: 1: 147:Boulton & Paul Overstrand 135:Central Landing Establishment 127: 588:Aircraft first flown in 1942 219: 7: 323: 292:295 lb (133.8 kg) 10: 604: 447:British Prototype Aircraft 164:Air Ministry Specification 517: 286:76 lb (34.5 kg) 45: 36: 31: 335: 445:Sturtivant, Ray. 1995. 418:"Museum of Army Flying" 259:General characteristics 143:De Havilland Tiger Moth 359:Sturtivant 2007, p. 38 228: 153:Design and development 330:Focke-Achgelis Fa 330 233:Museum of Army Flying 227: 206:RAF Sherburn-in-Elmet 178:Avro/Cierva C.30 Rota 296:Main rotor diameter: 182:Air Force Cross (UK) 114:Hafner H.8 Rotachute 171:Operational history 229: 565: 564: 461:Aeroplane Monthly 422:aviationmuseum.eu 137:(CLE) located at 110: 109: 32:Hafner Rotachute 16:(Redirected from 595: 503: 496: 489: 480: 479: 433: 432: 430: 428: 414: 408: 407: 405: 403: 388: 382: 379: 360: 357: 312: 302:Main rotor area: 261: 214:Hafner Rotabuggy 103: 67: 59:Type of aircraft 41: 29: 28: 21: 603: 602: 598: 597: 596: 594: 593: 592: 568: 567: 566: 561: 513: 507: 470: 442: 437: 436: 426: 424: 416: 415: 411: 401: 399: 389: 385: 380: 363: 358: 343: 338: 326: 308: 257: 249: 222: 186:barrage balloon 173: 155: 130: 101: 66:National origin 65: 60: 23: 22: 15: 12: 11: 5: 601: 591: 590: 585: 580: 563: 562: 560: 559: 554: 549: 544: 539: 534: 529: 524: 518: 515: 514: 506: 505: 498: 491: 483: 477: 476: 469: 468:External links 466: 465: 464: 457: 441: 438: 435: 434: 409: 383: 361: 340: 339: 337: 334: 333: 332: 325: 322: 321: 320: 317:Maximum speed: 306: 305: 299: 293: 287: 281: 275: 269: 248: 245: 221: 218: 198:RAF Chelveston 172: 169: 154: 151: 129: 126: 108: 107: 104: 98: 97: 94: 90: 89: 86: 82: 81: 76: 72: 71: 68: 62: 61: 58: 52: 48: 47: 43: 42: 34: 33: 9: 6: 4: 3: 2: 600: 589: 586: 584: 581: 579: 576: 575: 573: 558: 555: 553: 550: 548: 545: 543: 540: 538: 535: 533: 530: 528: 525: 523: 520: 519: 516: 511: 504: 499: 497: 492: 490: 485: 484: 481: 475: 472: 471: 462: 458: 456: 452: 448: 444: 443: 423: 419: 413: 398: 394: 387: 378: 376: 374: 372: 370: 368: 366: 356: 354: 352: 350: 348: 346: 341: 331: 328: 327: 318: 315: 314: 313: 311: 303: 300: 297: 294: 291: 290:Gross weight: 288: 285: 284:Empty weight: 282: 279: 276: 273: 270: 267: 264: 263: 262: 260: 255: 253: 244: 242: 238: 237:Middle Wallop 234: 226: 217: 215: 209: 207: 201: 199: 195: 190: 187: 183: 179: 168: 165: 161: 150: 148: 144: 140: 136: 125: 123: 119: 115: 105: 100: 99: 95: 92: 91: 87: 85:First flight 84: 83: 80: 77: 74: 73: 69: 64: 63: 57: 53: 50: 49: 44: 40: 35: 30: 27: 19: 551: 510:Raoul Hafner 460: 446: 440:Bibliography 425:. Retrieved 421: 412: 400:. Retrieved 396: 386: 381:Jarrett 1991 316: 309: 307: 301: 295: 289: 283: 277: 271: 265: 258: 256: 254:Jarrett 1991 251: 250: 230: 210: 202: 191: 174: 156: 131: 122:Raoul Hafner 120:designed by 113: 111: 102:Number built 79:Raoul Hafner 26: 578:Rotor kites 310:Performance 139:RAF Ringway 572:Categories 455:1856482219 128:Background 118:rotor kite 56:rotor kite 557:Rotabuggy 552:Rotachute 449:. Haynes 252:Data from 220:Survivors 189:gravity. 93:Produced 75:Designer 18:Rotachute 512:aircraft 324:See also 160:Bren gun 532:A.R.III 427:1 March 402:1 March 278:Height: 272:Length: 241:England 54:manned 537:A.R.IV 453:  542:A.R.V 336:Notes 266:Crew: 239:, in 106:c. 8 96:1942 88:1942 51:Role 547:PD.6 527:R.II 451:ISBN 429:2019 404:2019 112:The 522:R.I 70:UK 574:: 420:. 395:. 364:^ 344:^ 243:. 235:, 149:. 124:. 502:e 495:t 488:v 431:. 406:. 268:1 20:)

Index

Rotachute

rotor kite
Raoul Hafner
rotor kite
Raoul Hafner
Central Landing Establishment
RAF Ringway
De Havilland Tiger Moth
Boulton & Paul Overstrand
Bren gun
Air Ministry Specification
Avro/Cierva C.30 Rota
Air Force Cross (UK)
barrage balloon
Airborne Forces Experimental Establishment
RAF Chelveston
RAF Sherburn-in-Elmet
Hafner Rotabuggy

Museum of Army Flying
Middle Wallop
England
Focke-Achgelis Fa 330





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