“MAC Mamba”的意思、由来-开放百科全书

词条

MAC Mamba

释义

Design and development
Variants
Specifications (Prototype)
See also
References
Notes Bibliography

name=Mamba

image=

caption=

}}{{Infobox aircraft type

type=Two-seat light cabin monoplane

national origin=Australia

manufacturer=Melbourne Aircraft Corporation (Mamba Aircraft Company)
Australian Aircraft Industries

designer= Jess Smith^[1]

Stress Engineer Merv Reed

first flight=25 January 1989

introduced=

retired=

status=development continuing

produced=

primary user=

number built= 4

developed from=

variants with their own articles=

developed into= civil and military
}}

The MAC Mamba, Mamba Range is an Australian two-seat light aircraft designed and built by the Melbourne Aircraft Corporation.

Design and development

The Mamba is a strut-braced, high-wing monoplane designed over two years and first flown on 25 January 1989. It has fixed tricycle landing gear and is powered by a {{convert|116|hp|kW|0|abbr=on}} Lycoming O-235 flat-four piston engine. It has an enclosed glazed cabin with side-by-side configuration seating for two. The fuselage is constructed of welded steel tubing with stressed aluminum skin.^[1] It was intended to introduce four-seat and military versions of the Mamba.

The military version was built under contract by Australian Aircraft Industries as the AA-2S Mamba powered by a IO-360.{{citation needed|date=December 2013}}

Variants

AA-2

Lycoming O-235-powered prototype built by Melbourne Aircraft Corporation

AA-2M

Lycoming IO-360-powered military variant built by Australian Aircraft Industries

AA-2S

Lycoming IO-360-powered civilian under test by Mamba Aircraft Company

AA-4S

Lycoming O-320 four-place under development by Mamba Aircraft Company

Specifications (Prototype)

{{aerospecs
|ref=Jane's All the World's Aircraft 1989-90
|met or eng?=met
|genhide=
|crew=one
|capacity=one
|length m=7.00
|length ft=22
|length in=11½
|span m=8.68
|span ft=28
|span in=5¾
|height m=2.38
|height ft=7
|height in=9¾
|wing area sqm=10.13
|wing area sqft=109.04
|empty weight kg=390
|empty weight lb=860
|gross weight kg=680
|gross weight lb=1499 AA-2
|eng1 number=1
|eng1 type=Lycoming O-235-N2C flat-four piston engine
|eng1 kw=86
|eng1 hp=116
|eng2 number=
|eng2 type=
|perfhide=
|max speed kmh=250
|max speed mph=155
|range km=
|range miles=
|endurance h=5
|endurance min=42
|ceiling m=
|ceiling ft=
|climb rate ms=
|climb rate ftmin=1500
}}

References

Notes

1. ^¹{{cite journal|magazine=Air Progress|date=August 1989|page=26}}

Bibliography

{{cite book |editor-last= Taylor|editor-first= John W.R. |authorlink= |title= Jane's All the World's Aircraft 1989-90|year= 1989|publisher= Jane's Yearbooks |location=London, United Kingdom|isbn=0-7106-0896-9}}

4 : Australian civil utility aircraft 1990–1999|High-wing aircraft|Single-engined tractor aircraft|MAC aircraft

随便看