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词条 Solar MS-1
释义

  1. Specifications (MS-1)

  2. Notes

  3. References

name= MS-1 image= caption=

}}{{Infobox Aircraft Type

type= Airliner national origin= United States manufacturer= Solar Aircraft Company designer= William L. Lewis [1] first flight=21 January 1930[1] introduced= retired= status= primary user= number built= 1 developed from= Prudden SE-1 variants with their own articles=
}}

The Solar MS-1 was a prototype airliner built in the United States in 1930. It was a sesquiplane design, its wings braced to each other with warren truss-style struts. The stubby lower wings carried the divided main units of the fixed undercarriage. The fuselage was of rectangular cross-section and featured a fully enclosed flight deck and passenger cabin. The tail was of conventional design with strut-braced stabilizers and carrying a fixed tailwheel. Construction was of metal throughout,[2] and the aircraft was powered by a single radial engine in the nose.

The MS-1, registered X258V, flew for the first time on 21 January 1930 with Doug Kelly at the controls.[1] Kelly described it as "one of the finest closed planes I have ever flown",[1] and Charles Lindbergh also praised the MS-2 when he flew it a few days later.[1] Despite this, airlines did not order the type, although Northwest Airways considered buying ten examples.[1] Solar made the prototype available for charter types for a while, but in 1931 sold it to an operator in Mexico who used it to transport coffee beans.[1] On the Mexican register as XB-AFK, the MS-1 was destroyed in a crash in 1936.[2]

Specifications (MS-1)

{{Aircraft specs
|ref=Jane's all the World's Aircraft 1931[3], U.S. Commercial Aircraft[1]
|prime units?=imp


|crew=2
|capacity=8 pax
|length ft=35
|length in=11
|span ft=56
|span in=6
|height ft=10
|height in=2
|wing area sqft=496.5
|aspect ratio=
|airfoil=
|empty weight lb=3650
|gross weight lb=7000
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{cvt|135|USgal|impgal l}}
|more general=


|eng1 number=1
|eng1 name=Pratt & Whitney R-1340 Wasp
|eng1 type=9-cylinder air-cooled radial piston engine
|eng1 hp=420
|prop blade number=2
|prop name=fixed pitch metal propeller
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|max speed mph=130
|cruise speed mph=115
|cruise speed note=

  • Landing speed: {{cvt|60|mph|kn km/h}}
    |stall speed mph=
    |stall speed note=
    |never exceed speed kmh=
    |never exceed speed mph=
    |never exceed speed kts=
    |never exceed speed note=
    |range miles=
    |range nmi=
    |range note=
    |endurance=
    |ceiling ft=15000
    |ceiling note=service
    |g limits=
    |roll rate=
    |climb rate ftmin=750
    |climb rate note= initial
    |time to altitude=
    |wing loading lb/sqft=14
    |wing loading note=
    |fuel consumption lb/mi=
    |power/mass={{cvt|16.4|lb/hp|kg/kW}}
    |more performance=
    }}

    Notes

    1. ^Munson 1982, p.49
    2. ^"MS-1" at aerofiles
    3. ^{{cite book |title=Jane's all the World's Aircraft 1931 |editor1-last=Grey |editor1-first=C.G. |year=1931 |publisher=Sampson Low, Marston & company, ltd |location=London }}

    References

    • {{cite web |title=MS-1 |work=Aerofiles |url=http://www.aerofiles.com/_sk.html |accessdate=2011-02-27}}
    • {{cite book |last= Munson |first= Kenneth |title=U.S. Commercial Aircraft |year=1982 |publisher=Jane's |location=London |pages=49, 212 }}
    • {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=829 }}

    4 : United States airliners 1930–1939|Sesquiplanes|Single-engined tractor aircraft|Aircraft first flown in 1930

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