29:
189:. Both aircraft competed to be selected to meet the NBMR-3 requirement. While the Mirage IIIV is commonly viewed as being more politically palatable due to an emphasis having been placed upon multinational development and manufacturing plans, the design of P.1154 (which only used a single engine) was seen as more straightforward and practical. Ultimately the P.1154 was selected to meet the NBMR-3 requirement to the detriment of the Mirage IIIV. One of the two prototypes constructed was destroyed in an accident; shortly following its loss, the whole project was abandoned; the surviving aircraft has since been placed on public display.
311:, a key goal for the Balzac prototype was to prove the autopilot system, which was identical to the unit which was proposed use with the Mirage IIIV, as well as the lift and transition system. The Balzac began tethered hovering on 12 October 1962 and achieved the first free hover only six days later. The first accelerating transition from vertical take-off to horizontal flight took place on its 17th sortie on 18 March 1963. The aircraft had two fatal accidents, one in January 1964 and one in September 1965. After the last accident the aircraft was not repaired.
418:
320:
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266:(BAC), while the Dassault-led design also held the favour of several members of the British Air Staff. While the P.1154 was judged to be technically superior, the Mirage IIIV had acquired a greater level of political palatability due to the co-operative development and production aspects proposed for the programme, under which work was to be distributed across a number of member nations.
394:) fighter aircraft. It shared the general layout of earlier Mirage fighters, but featured a long and relative broad fuselage along with a bigger wing; the Mirage IIIV was considerably larger than contemporary fighter aircraft of its era. Akin to the earlier Balzac V testbed, the Mirage IIIV was outfitted with a total of nine engines: a single
426:
aircraft. As the engines accelerated to full power, these doors would automatically drop to a 90° position in order to obtain maximum lift thrust. According to Flight
International, the Mirage IIIV had an advertised performance envelope in the vicinity of Mach 1.15 when flown at low altitude and Mach 2.3 when flown at height.
270:
design did not lead to orders being placed for it. NATO lacked any central budget, instead relying on individual member nations to actually procure military equipment, contributing to the NBMR.3 selection going unheeded by all of the NATO member nations. Thus, in 1965, the NMBR.3 project was unceremoniously terminated.
1777:
Because it was a VTOL plane it could take off without doing a carrier launch or a normal takeoff like commercial airliners .e.g. A320neo takeoff... VTOL also means
Vertical Takeoff And Landing Such as the F-35 Lightning it costs around 109 million US dollars and it is very powerful and useful. Bogege
429:
Throughout development, the electronics were given substantial attention; it was this element of the design that has been attributed as being a major contributing factor to the cost overruns which impacted the programme. Many elements of the cockpit and ancillary electronics of the Mirage IIIV were
425:
A key design feature of the Mirage IIIV to improve vertical flight performance was the installation of movable thrust deflector doors ahead of the nozzles set in the aircraft's underside. These would be inclined 45° rearwards while on the ground, dispersing both debris and hot gasses away from the
365:
The loss of the second prototype had effectively killed the program, and in fact killed any prospect of an operational Mach 2 vertical take-off fighter for decades. The competing Hawker P.1154 had been cancelled in 1965 by the government just as the prototypes were under construction; however, its
269:
In May 1962, the proposed P.1154 emerged as the winner of the NBMR.3 competition . According to aviation author
Jeffort, the Mirage IIIV was rejected mainly because of its excessive complexity: using nine engines, compared to the P.1154's single-engine approach. However, the success of the P.1154
327:
Work on the Balzac assisted with the construction of the first prototype of the Mirage IIIV. This was roughly twice the size of the earlier aircraft. A pair of Mirage IIIV prototypes were constructed, the first of which conducted its first hovering trial on 12 February 1965. It was powered by a
210:
of 460 kilometres (250 nmi). Cruise speed was to be Mach 0.92, with a dash speed of Mach 1.5. The aircraft, with a 910-kilogram (2,000 lb) payload, had to be able to clear a 15-metre (50 ft) obstacle following a 150-metre (500 ft) takeoff roll. Victory in this
246:
was produced; however, the release of NBMR-3, and subsequent revisions to it, led to the P.1150 proposal being considered to be undersized and thus unsatisfactory, which led to a desire for a redesign. The new, larger aircraft design soon emerged, which was initially designated as
362:), conducted its first flight. During September of that year, it attained Mach 2.04 in level flight, but was lost in an accident on 28 November 1966. The Mirage IIIV was never able to take off vertically and successfully attain supersonic flight during the same flight.
343:, which shared many similarities to basic design of the Mirage IIIC design, with the exception of modifications in order to accommodate the selected engine. The TF104 engine was quickly replaced by an upgraded TF106 engine, with thrust of 74.5 kN (16,750 lb
262:. NBMR.3 attracted a total of eleven contenders, including Dassault's Mirage IIIV proposal, which would become viewed as the principal competitor to the P.1154. Substantial support for the Mirage IIIV came from Britain, work on the programme having involved the
370:
VTOL attack aircraft was flying in tri-partite trials with the UK, US and West
Germany. The French preferred the Mirage IIIV, and the international cooperation that would have been necessary to move the P.1154 into reality would never materialise.
291:
lift engines which had been specified for the Mirage IIIV were not expected to be available before 1963, Dassault decided to modify the first Mirage III prototype into an interim VTOL testbed; in this configuration, it became the
161:
which straddled the main engine. These lift jets would have been used during vertical takeoffs and landings, but would have been inactive during horizontal flight. The Mirage IIIV had come about as a response to the issuing of a
378:. The Mirage IIIV was never a realistic combat aircraft; the eight lift engines would likely have been a maintenance nightmare, and certainly their weight imposed a severe range and payload penalty on the aircraft.
1001:
273:
While the French government formally withdrew its participation in NMBR.3, after the Mirage IIIV had been rejected, Dassault continued work towards the building of Mirage IIIV prototypes.
222:(HSA) were deeply interested in vertical takeoff/landing (VTOL)-capable combat aircraft. HSA had already been keen to develop a new generation of combat aircraft that would be capable of
650:
According to aviation author Derek Wood, the decision not to persist with the original P.1150 design was a "serious setback...it would have provided a first class basic type".
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414:-1 engines, each being capable of generating a maximum of 15.7 kN (3,525 lbf) thrust, which were mounted vertically in pairs around the centreline.
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competition was viewed being of a high importance at the time as it was seem as being potentially "the first real NATO combat aircraft".
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Some of the P.1154 work contributed to the final operational vertical take-off fighter based on the
Kestrel, the highly successful
202:
In August 1961, NATO released an updated revision of its VTOL strike fighter requirement, NATO Basic
Military Requirement 3 (
28:
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347:), before the first prototype made its initial transition to forward flight in March 1966. The prototype subsequently attained
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decided that the company should investigate the prospects of developing and manufacturing a viable combat-capable
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936:. Vol. II: Military Prototype Aircraft from the Golden Age 1946–1974. Manchester, UK: Hikoki Publications.
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339:. The TF104 engine was originally evaluated on a specially-constructed aerial testbed aircraft, the
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Breffort, Dominique and Andre
Jouineau. "The Mirage III, 5, 50 and derivatives from 1955 to 2000."
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In
January 1962, HSA submitted the proposed design of the P.1154 to NATO via the
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later reused on the conventional Mirage IIIF, which later re-designated as the
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The Mirage IIIV was a VTOL derivative of an existing conventional fighter, the
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589:
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367:
235:
207:
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1035:. Warbird Tech. Vol. 21. North Branch, Minnesota: Specialty Press.
146:) prototype fighter aircraft of the mid-1960s developed and produced by
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579:
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319:
223:
206:). Specifications called for a supersonic V/STOL strike fighter with a
171:
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970:. Vol. 1: Post War Fighters. Manchester, UK: Crecy Publishing.
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engine cruise only, 88.26 kN (19,842 lbf) with afterburner
1326:
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508:
332:
158:
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turbofan engine for forward thrust of 82.4 kN (18,500 lb
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203:
167:
16:
French vertical take-off and landing prototype fighter aircraft
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engines, 19.61 kN (4,409 lbf) thrust each lift only
307:
BOr 3 as the main engine. According to aerospace publication
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During the 1950s and 1960, both French aircraft manufacturer
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51:
406:, capable of producing up to 61.8 kN (13,900 lb
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Dassault Mirage IIIV at Musée de l'Air et de l'Espace
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In June 1966, the second prototype, which featured a
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Aircraft of comparable role, configuration, and era
911:
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166:specification, NATO Basic Military Requirement 3 (
242:later on, a supersonic design, designated as the
234:(VTOL) fighter aircraft. Along with the subsonic
1782:
1062:. Madrid: Armas 30. Editorial San Martin, 1978.
1060:Mirage: Espejismo de la tĂ©cnica y de la polĂtica
906:
894:
142:, was a French vertical take-off and landing (
1009:. London: Royal Air Force Historical Society.
1383:
1101:
772:
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803:"Balzac VTOL Forerunner of the Mirage IIIV."
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954:. Paris: Histoire et Collections, 2004.
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226:speeds. HSA's chief aircraft designer
177:The Mirage IIIV was a competitor with
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778:Jefford 2006 et al., pp. 12–13.
276:
1816:Aircraft with auxiliary jet engines
617:List of military aircraft of France
390:-capable vertical takeoff/landing (
251:prior to being redesignated as the
13:
988:. London: Guild Publishing, 1985.
986:Modern Combat Aircraft 23 - Mirage
966:Carbonel, Jean-Christophe (2016).
479:5.55 m (18 ft 3 in)
473:8.72 m (28 ft 7 in)
446:Modern Combat Aircraft 23 - Mirage
14:
1832:
1074:
300:lift engines along with a single
769:Jefford 2006 et al., p. 19.
670:Jefford 2006 et al., p. 12.
537:
493:Pratt & Whitney/SNECMA TF104
467:18 m (59 ft 1 in)
238:fighter (which would become the
27:
925:
864:
849:
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485:12,000 kg (26,455 lb)
438:Specifications (Mirage IIIV-01)
386:The Dassault Mirage IIIV was a
1489:MD.750 Mirage 6000 Mega Mirage
644:
218:and British aerospace company
185:VTOL fighter, a cousin of the
174:-capable VTOL strike fighter.
1:
1801:1960s French fighter aircraft
808:, 2 August 1962. pp. 174-175.
632:
296:. This was fitted with eight
232:vertical take-off and landing
197:
35:Musée de l'Air et de l'Espace
1821:Aircraft first flown in 1965
1796:Tailless delta-wing aircraft
1058:PĂ©rez, San Emeterio Carlos.
846:, 25 February 1965. p. 276.
657:
264:British Aircraft Corporation
7:
1055:, 20 May 1965. pp. 774–775.
530:
10:
1837:
1031:Jenkins, Dennis R (1998).
1000:Jefford, C.G, ed. (2006).
746:Buttler 2000, p. 119.
714:Buttler 2000, p. 118.
351:1.32 during test flights.
335:engine, designated as the
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1811:Nine-engined jet aircraft
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1339:
1319:
1303:
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1081:Dassault Mirage IIIV page
891:20 May 1965, pp. 774-775.
861:, Retrieved 18 June 2017.
400:Pratt & Whitney JTF10
381:
330:Pratt & Whitney JTF10
122:
111:
103:
98:
90:
80:
72:
60:
47:
42:
26:
21:
637:
622:List of fighter aircraft
220:Hawker Siddeley Aviation
1791:Dassault Group aircraft
723:Wood 1975, pp. 211-213.
585:Hawker Siddeley Harrier
452:General characteristics
410:) of thrust, and eight
368:Hawker-Siddeley Kestrel
240:Hawker Siddeley Harrier
187:Hawker Siddeley Harrier
1632:New Generation Fighter
1347:Australian procurement
968:French Secret Projects
932:Buttler, Tony (2015).
793:, 17 May 1962. p. 764.
422:
324:
315:Mirage IIIV prototypes
193:Design and development
1003:The RAF Harrier Story
876:, 6 May 1965. p. 687.
841:"IIIV in the Z Axis."
627:List of VTOL aircraft
496:afterburning turbofan
420:
402:turbofan, designated
366:subsonic cousin, the
322:
1053:Flight International
918:20 May 1965, p. 775.
916:Flight International
903:20 May 1965, p. 774.
901:Flight International
889:Flight International
874:Flight International
844:Flight International
831:Jackson 1985, p. 66.
817:Jackson 1985, p. 62.
806:Flight International
791:Flight International
323:Dassault Mirage IIIV
309:Flight International
260:Ministry of Aviation
136:Dassault Mirage IIIV
37:, Le Bourget, France
1225:MD550 Mystère Delta
952:Planes and Pilots 6
788:"R-R for Dassault."
563:Dassault Mirage III
552:Related development
155:Dassault Mirage III
43:General information
33:Mirage IIIV at the
1033:Boeing/BAe Harrier
934:X-Planes of Europe
760:Wood 1975, p. 216.
732:Wood 1975, p. 213.
690:Wood 1975, p. 215.
568:Dassault Mirage F1
423:
325:
298:Rolls-Royce RB.108
170:), which sought a
76:Destroyed (France)
1773:
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1335:
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977:978-1-91080-900-6
943:978-1-90210-948-0
859:Dassault Aviation
558:Dassault Balzac V
506:Rolls-Royce RB162
412:Rolls-Royce RB162
289:Rolls-Royce RB162
283:Dassault Balzac V
277:Dassault Balzac V
216:Dassault Aviation
148:Dassault Aviation
132:
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127:Dassault Balzac V
67:Dassault Aviation
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871:"Snecma TF-106."
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1050:"Mirage IIIV."
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1042:1-58007-014-0
1038:
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1016:0-9530345-2-6
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994:0-7110-1512-0
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960:2-913903-92-4
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702:, p. 19.
701:
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611:Related lists
606:
603:
601:
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596:
593:
591:
590:Hawker P.1154
588:
586:
583:
581:
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490:
487:
484:
483:Gross weight:
481:
478:
475:
472:
469:
466:
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460:
457:
456:
455:
453:
448:
447:
444:
435:
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256:
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245:
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237:
236:Hawker P.1127
233:
229:
225:
221:
217:
212:
209:
208:combat radius
205:
190:
188:
184:
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175:
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46:
41:
36:
30:
25:
20:
1775:
1554:
1304:South Africa
1149:
1059:
1052:
1032:
1021:the original
1002:
985:
967:
951:
933:
926:Bibliography
915:
900:
896:
888:
873:
866:
858:
851:
843:
836:
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805:
798:
790:
783:
774:
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728:
719:
700:Jenkins 1998
695:
666:
646:
610:
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573:
572:
551:
550:
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243:
213:
201:
176:
152:
140:Mirage III V
139:
135:
133:
115:12 February
112:First flight
104:Manufactured
91:Number built
81:Primary user
62:Manufacturer
1617:Mystère III
1595:2000N/2000D
1530:Étendard VI
1525:Étendard IV
1520:Étendard II
517:Performance
502:Powerplant:
489:Powerplant:
341:Mirage IIIT
22:Mirage IIIV
1785:Categories
1693:Mystere 20
1688:Mystere 10
1678:Hirondelle
1673:Communauté
1622:Mystère IV
1612:Mystère II
1351:Operators
633:References
580:EWR VJ 101
398:-modified
388:supersonic
302:unreheated
287:Since the
224:supersonic
198:Background
172:supersonic
1607:Mystère I
1510:Alpha Jet
658:Citations
526:Mach 2.04
471:Wingspan:
443:Data from
432:Mirage F1
159:lift jets
107:1965-1966
1806:Lift jet
1515:Balzac V
1498:Military
1401:aircraft
1399:Dassault
1288:Pakistan
1220:Balzac V
1117:Dassault
531:See also
509:turbojet
333:turbofan
294:Balzac V
249:P.1150/3
1778:out...
1683:Mercure
1647:Spirale
1637:Ouragan
1540:Flamant
1407:Numeric
1311:Cheetah
1253:Pantera
477:Height:
465:Length:
376:Harrier
328:single
99:History
1698:Falcon
1642:Rafale
1627:nEUROn
1545:Mirage
1484:MD.610
1479:MD.550
1474:MD.455
1469:MD.454
1464:MD.453
1459:MD.452
1454:MD.450
1449:MD.415
1444:MD.410
1439:MD.320
1434:MD.316
1429:MD.315
1424:MD.312
1419:MD.311
1414:MD.303
1340:Topics
1279:Nesher
1274:Nammer
1262:Israel
1122:family
1120:Mirage
1066:
1039:
1013:
992:
974:
958:
940:
396:SNECMA
382:Design
253:P.1154
244:P.1150
204:NBMR-3
183:P.1154
168:NBMR-3
73:Status
1666:Civil
1246:Chile
1230:Milan
1024:(PDF)
1007:(PDF)
638:Notes
459:Crew:
404:TF104
356:TF306
337:TF104
1738:2000
1600:4000
1590:2000
1555:IIIV
1505:AFVG
1327:F-21
1295:ROSE
1269:Kfir
1204:6000
1199:4000
1187:2000
1064:ISBN
1037:ISBN
1011:ISBN
990:ISBN
972:ISBN
956:ISBN
938:ISBN
504:8 Ă—
491:1 Ă—
392:VTOL
349:Mach
164:NATO
144:VTOL
134:The
117:1965
52:VTOL
48:Type
1763:10X
1733:900
1728:200
1723:100
1550:III
1192:N/D
1145:III
181:'s
1787::
1758:8X
1753:7X
1748:6X
1743:5X
1718:50
1713:30
1708:20
1703:10
1580:F2
1575:F1
1570:50
1560:IV
1177:F2
1172:F1
1167:50
1157:IV
1140:II
908:^
881:^
822:^
751:^
737:^
707:^
675:^
434:.
255:.
150:.
1585:G
1565:5
1391:e
1384:t
1377:v
1182:G
1162:5
1150:V
1135:I
1109:e
1102:t
1095:v
1070:.
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996:.
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962:.
946:.
461:1
408:f
360:f
345:f
94:2
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
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