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<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{|{{Infobox Aircraft Begin
 | name=M 360 Jupiter
 | image=Moynet_Jupiter_F-BLKY_TNF_040671-1-.jpg
 | caption=The Moynet 360-6 second prototype Jupiter at Toussus-le-Noble airfield near Paris in June 1971. (Rear propeller is hidden by starboard fin.)
}}{{Infobox Aircraft Type
 | type=Executive transport
 | national origin=[[France]]
 | manufacturer=Engins Matra/[[Sud Aviation]]
 | designer=André Moynet
 | first flight=17 December 1963
 | introduced=
 | retired=
 | status=
 | primary user=
 | more users= <!--Limited to three in total; separate using <br /> -->
 | produced= <!--years in production-->
 | number built=2
 | program cost= <!--Total program cost-->
 | unit cost= <!--Incremental or flyaway cost for military or retail price for commercial aircraft-->
 | developed from=
 | variants with their own articles=
}}
|}

The '''Moynet M 360 Jupiter''' was a small executive transport built in France in the 1960s.  It had an unusual twin-[[push-pull configuration|push-pull]], single-[[fuselage]] configuration. Two prototypes were produced, the second with more power and seating, but no sales resulted.

==Design and development==

Some civil propeller driven aircraft that have used one or more pairs of engines in [[Push–pull configuration|push-pull]] configuration have been flying boats, with engines mounted above the wing and clear of spray. Others have had a pair of engines, one at either end of a pod fuselage with a tail unit mounted on a pair of booms, for example the [[Cessna Skymaster]], the [[Adam A500]] or the [[Rutan Voyager]]. The Moynet 360 Jupiter was an example of a push-pull aircraft of a less common configuration, where a single conventional fuselage has an engine at either end; the [[Dornier Do 335]] fighter used the same arrangement.  For light civil aircraft, the aim was to combine the performance of a conventional twin-engined aircraft with the ease of handling of a single-engined one.<ref name="Flight 2">{{Harvnb|Lambert|1964|pp=1075–1077}}</ref>

The Jupiter was an executive transport with between four and seven seats, depending on engine power.  It was designed by André Moynet, a member of the [[National Assembly of France]] and a former government minister, while also a test-pilot,<ref>"[http://www.ordredelaliberation.fr/fr_compagnon/1057.html André Moynet]". ''www.ordredelaliberation.fr''. 15 October 2003. Retrieved 8 January 2010.</ref> and built by S.S. Engins Matra (so it is sometimes referred to as the '''Matra Moynet Jupiter'''<ref name="Flight 2"/>), the first prototype flying on 17 December 1963 with the designer and Lucien Tieles at the controls.<ref name="Flight">{{cite web|url=http://www.flightglobal.com/pdfarchive/view/1964/1964%20-%200136.html|title=''Flight'' 16 January 1964 p.93}}</ref>  Its wing had a straight trailing edge, but the centre section had strong taper on the leading edge which continued more weakly outboard.  It was of two spar, stressed skin construction, carrying mass balanced ailerons and slotted flaps.  The main undercarriage legs, placed at the end of the centre section each carried a single wheel and retracted inwards electrically.  A retractable nosewheel completed the landing gear.<ref name="JAWA66">{{harvnb|Taylor|1966|pp=60–1}}</ref>
[[File:Moynet 360-6 Jupiter F-BLKY Toussus 06.77 edited-3.jpg|thumb|right|The 360-6 Jupiter showing the fore and aft arrangement of the two engines with the rear power unit set between the twin fins.]]
One horizontally opposed Lycoming engine was conventionally placed in the nose.  Behind it was a standard cabin, though the front seats were further ahead of the leading edge than usual because of the rearward shift of the centre of gravity caused by the rear engine.  There were three large windows on each side. For the same reason the rear fuselage was quite short, and it lacked the normal taper, giving it a boxy look, so that the second, pusher Lycoming could be mounted in the extreme tail. This was cooled by air from rectangular intakes on the upper sides of the rear fuselage.  The straight edged, tapered tailplane was mounted on the fuselage top above the engine, with small endplate fins carrying balanced rudders.  These fins extended above and below the tailplane, with arrow shaped leading edges and straight, swept trailing edges.  There was also a long, shallow strake over the rear fuselage. Seen from below, the long span of the tailplane was striking, about 44% of that of the wings; the elevators filled most of the outer part of its trailing edge, avoiding the propeller airstream.<ref name="JAWA66"/>

Only two Jupiters were built. The first, designated 360-4 and initially registered as ''F-WLKE'' had two 200&nbsp;hp (150&nbsp;kW) [[Lycoming O-360|Lycoming IO-360-A1A]] engines driving two-bladed propellers and was configured as a 4-5 seater.<ref name="OBA">{{harvnb|Green|1964|pp=170–1}}</ref>

The second prototype was of a more powerful and slightly larger variant designated the model 360-6; it first flew on 25 May 1965.<ref name="Janes 65 p60-1">{{harvnb|Taylor|1965|p=60}}</ref>   This model had a choice of engines, either 290&nbsp;hp (216&nbsp;kW) [[Lycoming IO-540]] six cylinder engines driving constant speed, three-bladed propellers, or 310&nbsp;hp (231&nbsp;kW) [[Lycoming TIO-541]] engines.  The span was increased by 0.37 m (15&nbsp;in) and length by 0.64 m (25&nbsp;in).<ref name="JAWA66"/><ref name="OBA"/>  The increased length allowed seats for 6-7, with two rows of two single seats and a bench seat at the rear that could accommodate 2 or 3.  The cabin was sound-proofed and air conditioned and could be pressurised.  Access was via a forward starboard side door.  There was baggage space behind the cabin with its own external door.  The sole 360-6 was registered as ''F-WLKY''.<ref name="JAWA66"/>

The intention was for Sud-Aviation to produce the 360-6 Jupiter as the '''Sud-Aviation M 360-6 Jupiter'''.<ref name="JAWA66"/>  An order was obtained from the French government for some 360-6 pre-production aircraft,<ref name="JAWA66"/> but this seems to have been cancelled.  Despite sales campaigns in Europe and the United States no further orders resulted.<ref name="1000 air">Visschedijk, Johan. "[http://www.1000aircraftphotos.com/HistoryBriefs/Moynet360Jupiter.htm Moynet M 360-4 Jupiter]". ''[http://www.1000aircraftphotos.com/ 1000AIRCRAFTPHOTOS.COM]''. 23 March 2004. Retrieved 8 January 2009.</ref>

The first prototype is now in the reserve collection of the [[Musée de l'Air et de l'Espace]], [[Le Bourget Airport]], [[Paris]] museum and the second in the [[Musée Regional de l'Air]],<ref>{{cite web|url=http://www.aviationmuseum.eu/World/Europe/France/Angers/musee_regional_air_gppa.htm|title=Musee Regional de l'Air - GPPA - Angers - France|website=www.aviationmuseum.eu}}</ref> [[Angers - Loire Airport]], [[France]], having been restored to flying condition in 2018.<ref name="aero521p76">{{harvnb|Halford|2021|p=76}}</ref> At le Bourget, the 360-4 bears the normal [[Aircraft registration#List of countries/regions and their registration prefixes and patterns|French registration]]'' F-BLKE'' rather than the French prototype style ''F-WLKE''.
<!-- ==Operational history== -->

==Variants==
;M 360-4 Jupiter
:First prototype, 4–5 seats, two 149&nbsp;kW (200&nbsp;hp) [[Lycoming O-360|Lycoming IO-360]] engines.<ref name="Flight"/><ref name="Janes 65 p60-1"/>
;M 360-6
:Second prototype, with stretched fuselage with seven seats and two 216&nbsp;kW (290&nbsp;hp) [[Lycoming O-540|Lycoming IO-540]] engines.<ref name="Flight"/><ref name="Janes 65 p60-1"/>
;M 360-6P
:Proposed [[Cabin pressurization|pressurised]] seven-seat version, with [[Lycoming O-480]] engines.  Unbuilt.<ref name="Janes 65 p60-1"/>
;Sud-Aviation Présidence
:Further enlarged, pressurised version planned by Sud-Aviation.<ref name="1000 air"/>
<!-- ==Units using this aircraft/Operators (choose)== -->

==Specifications (360-6, Lycoming IO-540) ==
{{Aircraft specs
|ref={{harvnb|Taylor|1966|pp=60–1}}
|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->
<!--
        General characteristics
-->
|genhide=
|crew=
|capacity=6 or 7 including crew
|length m=8.77
|length ft=
|length in=
|length note=
|span m=11.49
|span ft=
|span in=
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|mid span m=
|mid span ft=
|mid span in=
|mid span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|swept m=<!-- swing-wings -->
|swept ft=<!-- swing-wings -->
|swept in=<!-- swing-wings -->
|swept note=
|dia m=<!-- airships etc -->
|dia ft=<!-- airships etc -->
|dia in=<!-- airships etc -->
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|width m=<!-- if applicable -->
|width ft=<!-- if applicable -->
|width in=<!-- if applicable -->
|width note=
|height m=2.46
|height ft=
|height in=
|height note=
|wing area sqm=16.81
|wing area sqft=
|wing area note=
|swept area sqm=<!-- swing-wings -->
|swept area sqft=<!-- swing-wings -->
|swept area note=
|volume m3=<!-- lighter-than-air -->
|volume ft3=<!-- lighter-than-air -->
|volume note=
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight kg=1338
|empty weight lb=
|empty weight note=
|gross weight kg=2390
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=566 L
|lift kg=<!-- lighter-than-air -->
|lift lb=<!-- lighter-than-air -->
|lift note=
|more general=
<!--
        Powerplant
-->
|eng1 number=2
|eng1 name=[[Lycoming IO-540]]
|eng1 type=6-cylinder horizontally opposed air cooled
|eng1 kw=216<!-- prop engines -->
|eng1 hp=<!-- prop engines -->
|eng1 kn=<!-- jet/rocket engines -->
|eng1 lbf=<!-- jet/rocket engines -->
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=<!-- afterburners -->
|eng1 lbf-ab=<!-- afterburners -->
|eng2 number=
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|eng2 kw=<!-- prop engines -->
|eng2 hp=<!-- prop engines -->
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|eng2 lbf-ab=<!-- afterburners -->
|eng3 number=
|eng3 name=
|eng3 type=
|eng3 kw=<!-- prop engines -->
|eng3 hp=<!-- prop engines -->
|eng3 kn=<!-- jet/rocket engines -->
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|eng3 note=
|eng3 kn-ab=<!-- afterburners -->
|eng3 lbf-ab=<!-- afterburners -->
|more power=
|prop blade number=3<!-- propeller aircraft -->
|prop name=Hartzell constant speed
|prop dia m=<!-- propeller aircraft -->
|prop dia ft=<!-- propeller aircraft -->
|prop dia in=<!-- propeller aircraft -->
|prop note=
|rot number=<!-- helicopters -->
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<!--
        Performance
-->
|perfhide=
|max speed kmh=363
|max speed mph=
|max speed kts=
|max speed note=at sea level.  All performance figures estimates at maximum take-off weight.
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=338
|cruise speed mph=
|cruise speed kts=
|cruise speed note=at 1,830 m (6,000 ft) on 75% power
|stall speed kmh=<!-- aerobatic -->
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|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
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|minimum control speed mph=
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|minimum control speed note=
|range km=2060
|range miles=
|range nmi=
|range note=at 4,500 m(15,000 ft) and 45% power.
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
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|endurance=<!-- if range unknown -->
|ceiling m=
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|g limits=<!-- aerobatic -->
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|glide ratio=<!-- sailplanes -->
|climb rate ms=7.3
|climb rate ftmin=
|climb rate note=at sea level
|time to altitude=
|sink rate ms=<!-- sailplanes -->
|sink rate ftmin=<!-- sailplanes -->
|sink rate note=
|lift to drag=
|wing loading kg/m2=
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|disk loading kg/m2=
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<!--
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-->
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|avionics=
}}

==See also==
{{aircontent
<!-- include as many lines are appropriate. additional lines/entries with carriage return. -->
|see also=
|related=<!-- related developments -->
|similar aircraft=*[[Cessna Skymaster]]
*[[Adam A500]]<!-- similar or comparable aircraft -->
|lists=<!-- related lists -->
}}

==References==

===Citations===
{{Reflist}}

===Cited sources===

*{{cite book |title= Observer's Book of Aircraft|last=Green |first= William |year= 1964|publisher=Frederick Warne & Co. Ltd.|location= London}}
*{{cite magazine |last=Halford |first=David |title=Jupiter Ascending |magazine=[[Aeroplane Monthly|Aeroplane]] |date=May 2021 |volume=49 |issue=5 |pages=72–78 |issn=0143-7240}}
* {{cite magazine|last=Lambert|first=Mark|title=In The Air:No 187: Matra-Moynet Jupiter|magazine=[[Flight International]]|date=25 June 1964| url=http://www.flightglobal.com/pdfarchive/view/1964/1964%20-%201952.html|pages=1075–1077}} 
* {{cite magazine |last=Ravel |first=Christian |title=Le Moynet 360 "Jupiter" du musée Espace Air Passion: Un retour sensationnel |magazine=Le Fana de l'Aviation |issue=619 |date=June 2021 |pages=36–46 |language=fr |issn=0757-4169}}
*{{cite journal |last1=Simpson |first1=Rod |title=The Faster Skymaster|journal=The Aviation Historian |date=January 2013 |issue=2 |pages=102–109 |issn=2051-1930}}
*{{cite book |title= Jane's All the World's Aircraft 1965-66|last= Taylor |first= John W R |year=1965|publisher= Sampson Low, Marston &Co. Ltd|location= London}}
*{{cite book |title= Jane's All the World's Aircraft 1966-67|last= Taylor |first= John W R |year=1966|publisher= Sampson Low, Marston &Co. Ltd|location= London}}

==External links==
*[http://www.1000aircraftphotos.com/Contributions/Visschedijk/3373L.jpg Photo of 360-4]

[[Category:1960s French civil utility aircraft]]
[[Category:Twin-engined push-pull aircraft]]
[[Category:Aircraft first flown in 1963]]
[[Category:Low-wing aircraft]]
[[Category:Twin-tail aircraft]]

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