View source for Aeroput MMS-3

{|{{Infobox aircraft begin
|name=Aeroput MMS-3
|image=Avion aeroput mms-3.jpg
|caption=
}}
{{Infobox aircraft type
|type=Light transport / Utility
|national origin=[[Serbia]]
|manufacturer=Aeroput workshops, [[Zemun]], [[Serbia]]
|designer=Milenko Mitrović - Spirta
|first flight=January 1936
|introduced=
|retired=
|status= Destroyed
|primary user=[[Aeroput]]
|more users=
|produced=
|number built=1
|variants with their own articles=
}}
|}
The '''Aeroput MMS-3'''  ({{Lang-sr-Cyrl|Аеропут ММС-3}}) was the first Yugoslavian twin-engined light three-seater passenger aircraft, produced by Aeronautical service of [[Aeroput]] for its own needs in 1935. The chief designer was the aviation engineer Milenko Mitrović - Spirta, the [[Chief technology officer|CTO]] of Aeroput.
==Development==
Design work was conducted in 1934, the designer was aeronautical engineer Milenko Mitrović - Spirta, whose initials are on the plane as the MMS label (such was then the custom among constructors of Yugoslav aircraft). The number on the label represents a 3-seater passenger plane. Mr Milenko Mitrović - Spirta was then technical director of Aeroput and suggested that the Board of Directors on the basis of his project, which was in March 1934 tested in the [[Subsonic and transonic wind tunnel|Eiffel wind tunnel]] in Paris, made for Aeroput in his workshop for repairing aircraft an airplane which would be used as aviotaxi, for whom he felt a great need. The constructor then tried several configurations, including inline and radial engines, without guards and shields, placed at different distances from the fuselage. The final configuration was characterised by an aerodynamic perfection of Class 12, in those years achieved only by very good gliders. During 1935 the prototype was built, the maiden flight occurring in January 1936. The first flight and test of the aircraft were conducted by pilot [[Vladimir Strzhizhevsky|Vladimir Striževski]], head of Aeroput transport pilots. As the plane showed good performance, in the same season in 1936 it entered operational use.
==Technical specification==
The MMS-3 was a twin-engine high-wing monoplane of wooden construction with the fuselage covered with plywood, and the wings with fabric, intended primarily for aerial taxi operations. It was powered by two 88&nbsp;hp (66&nbsp;kW; 90 PS) [[Pobjoy Niagara|Pobjoy Niagara III]] 7-cylinder piston radial engines, driving two-bladed fixed-pitch propellers. These engines were characterized by low fuel consumption and very quiet operation, allowing greater passenger comfort. For that time the plane had unusual concept, instead of conventional fuselage, in the extension of the engine carrier had two tail fins (bi-fuselage). Fuel tanks were located in the wing between the two engines with fuel capacity of {{convert|265|L|gal|abbr=on|0}}. Cabins of pilots and passengers represent one unit, which like gondola is located below the airplane wings.
The cabin had a large window area that provided excellent visibility to the pilot and passengers. This made it an extraordinary airplane for panorama flights. The plane had fixed landing gear of a conventional type, with the tail wheel located at the rear of the fuselage and the main wheels mounted on one side of the gondola fuselage and on the other side to engine mount. The main wheels had aerodynamic fenders.<ref>{{Cite web|url=http://www.samoloty.ow.pl/str372.htm |title=Mitrović MMS-3 |publisher=www.samoloty.ow.pl |url-status=dead |archiveurl=https://web.archive.org/web/20100410033302/http://www.samoloty.ow.pl/str372.htm |archivedate=April 10, 2010 }}</ref> In 1940 year, the MMS-3 was used to test [[tricycle undercarriage]], i.e. with a nose wheel.<ref>{{Cite web|url=http://img403.imageshack.us/img403/4021/mms3.jpg |title=The MMS-3 in April 1940 during the test of the tricycle undercarriage with the front wheel |url-status=bot: unknown |archiveurl=https://web.archive.org/web/20131111115606/http://img403.imageshack.us/img403/4021/mms3.jpg |archivedate=2013-11-11 }}</ref> During this time the engineer Mitrović and Prof. Dr. Ing. [[Miroslav Nenadović]] collaborated on a twin engine light bomber project called Nemi, and that was supposed to have a similar arrangement as used on the MMS-3, but with a tricycle undercarriage. The project Nemi was never realised.
The appearance of plane Aeroput MMS-3, because of its outstanding aerodynamic characteristics, caused a great interest in France, United Kingdom, Germany and Czechoslovakia.{{citation needed|date=June 2021}} Negotiations for the sale of the license were started, but were not concluded, and no series production did ever take place.
==Operational use ==
In the summer of 1936 year the MMS-3 received a certificate and was registered as YU-SAR. It was used on passenger routes from [[Belgrade]] to [[Sarajevo]], [[Podgorica]] and [[Skoplje]], also carrying mail and newspapers. During a flight on the route [[Airport City Belgrade#Location|Belgrade]] – [[Batlava-Donja Penduha Airfield|Podujevo]] – [[Skopje Airport|Skoplje]] on 15 September 1936 it made a forced landing due to an engine failure and was damaged slightly. The damage was quickly repaired so that the aircraft, by the end of 1937, had completed 65 hours of flight time, 1938  – 79 hours, 1939  – 102 hours. In addition, it was used by Aeroput for pilot training. It was also used for publicity purposes, taking the visitors of aero-meetings for joy-rides at minimum prices which contributed to the popularisation of aviation and [[air transport in Yugoslavia]]. The plane had another advantage: passenger seats could be easily removed from the cabin and the plane turned into a cargo airplane (the first Yugoslav cargo plane).
Just before the [[April War]] in 1941 the aircraft was used by the 603rd training squadron of the [[Royal Yugoslav Air Force]] (JKRV) which was located at [[Bogojević Selo|Grab Airport]] near [[Trebinje]] and it was destroyed during withdrawal from the airport. According to other sources, in March 1941, in light of the tense international situation around Yugoslavia, the  MMS-3 aircraft was taken over by the JKRV and placed in the 603rd Auxiliary Squadron where it was to be used as a liaison aircraft for deployment and courier needs.
[[File:1941-Milenko.jpg|thumb|right|Milenko Mitrović Spirta with MMS-3, before he set it on fire, to prevent Germans taking it (1941).]]
According to eyewitness reports, after the German invasion of Yugoslavia in April 1941, the aircraft was destroyed by the crew at the [[Valjevo Airport|airport]] near the village of [[Divci (Valjevo)|Divci]] in [[Valjevo]] region so that it would not fall into enemy hands. The Plane constructor Milenko Mitrović Spirta (15 February 1905 [[Novi Sad]], Serbia - 23 August 1986 [[Peterborough, New Hampshire|Peterborough]], NH, USA) photographed the plane before it was destroyed.
==Operators==
===Civil operators===
;{{flag|Kingdom of Yugoslavia}}
* [[Aeroput]]
===Military operators===
;{{flag|Kingdom of Yugoslavia}}
* [[Royal Yugoslav Air Force]]
==Specifications (MMS-3)==
{{Aircraft specs
|ref=''all-aero.com - Aeroput MMS-3'' <ref name="allaero">{{cite web |title=Aeroput MMS-3 |url=http://all-aero.com/index.php/contactus/44-planes-a-b-c/13747-aeroput-mms-3 |website=all-aero.com |accessdate=20 August 2019 |archive-date=20 August 2019 |archive-url=https://web.archive.org/web/20190820163028/http://all-aero.com/index.php/contactus/44-planes-a-b-c/13747-aeroput-mms-3 |url-status=dead }}</ref>
|prime units?=met
<!--
General characteristics
-->
|crew=1
|capacity=3 passengers
|length m=7.42
|length note=
|span m=11.56
|span note=
|height m=2.25
|height note=
|wing area sqm=16
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil=
|empty weight kg=630
|empty weight note=
|gross weight kg=1030
|gross weight note=
|max takeoff weight kg=
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
Powerplant
-->
|eng1 number=2
|eng1 name=[[Pobjoy Niagara III]]
|eng1 type=7-cylinder air-cooled geared radial piston engines
|eng1 note={{cvt|66|kW|PS hp}}
|prop blade number=2
|prop name=wooden fixed-pitch propellers
|prop dia m=<!-- propeller aircraft -->
|prop dia note=
<!--
Performance
-->
|max speed kmh=235
|max speed note=
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=215
|cruise speed note=<br/>
*'''Landing speed:''' {{cvt|75|km/h|mph kn}}
|stall speed kmh=
|stall speed note=
|never exceed speed kmh=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed note=
|range km=600
|range note=
|combat range km=
|combat range note=
|ferry range km=
|ferry range note=
|endurance=3 hours (2 passengers); 5 hours (1 passenger)
|ceiling m=6000
|ceiling note=<br/>
::::{{cvt|1800|m}} (single engine)
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=6.5
|climb rate note=
|time to altitude={{cvt|5000|m}} in 22 minutes
|wing loading kg/m2=64.38
|wing loading note=
|fuel consumption kg/km=
|power/mass={{cvt|0.13|kW/kg}}
|more performance=
}}
==See also==
*[[Jat Tehnika]]
*[[Yugoslav Royal Air Force]]
==References==
{{reflist}}
==External links==
*[http://i1228.photobucket.com/albums/ee446/lleullaugiffin/Europa/Mitrovich-MMS-3-3-view-1.jpg The Aeroput MMS-3 three view drawing]
[[Category:1930s Yugoslav aircraft]]