“Summit 103 Mini Breeze”的意思、由来-开放百科全书

The Summit 103 Mini Breeze is an American powered parachute, designed and produced by Summit Aerosports of Yale, Michigan.^[1]

Design and development

The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of {{convert|254|lb|kg|0|abbr=on}}. The Mini Breeze has a standard empty weight of {{convert|240|lb|kg|0|abbr=on}} when equipped with a Rotax 447 engine and {{convert|253|lb|kg|0|abbr=on}} when equipped with a Rotax 503. It features a parachute-style high-wing, single-place accommodation, tricycle landing gear and a single {{convert|40|hp|kW|0|abbr=on}} Rotax 447 engine in pusher configuration. The {{convert|50|hp|kW|0|abbr=on}} Rotax 503 engine is a factory option.^[1]^[2]

The Mini Breeze's airframe is built from TIG-welded, powder coated 4130 steel tubing. The standard rectangular Mustang S-380 canopy has an area of {{convert|380|sqft|m2|abbr=on}} and is attached at four points to increase stability. The Mustang S-380 allows a gross weight of {{convert|550|lb|kg|0|abbr=on}}. Optional canopies include the elliptical Mustang E-280 and the elliptical Thunderbolt E-310 which both allow a gross weight of {{convert|600|lb|kg|0|abbr=on}}. In-flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has nosewheel steering controlled by a butterfly steering wheel and the main landing gear incorporates bungee suspension. The aircraft is factory supplied complete.^[1]^[2]

Specifications (103 Mini Breeze)

|genhide=
|crew=one
|capacity=
|length m=
|length ft=8
|length in=5
|length note=
|span m=
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=380
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=240
|empty weight note=
|gross weight kg=
|gross weight lb=550
|gross weight note=with Mustang S-380 wing
|fuel capacity={{convert|12|u.s.gal}}, limited to {{convert|5|u.s.gal}} under US ultralight rules
|more general=

|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=25
|cruise speed kts=
|cruise speed note=
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|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
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|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=4:1
|climb rate ms=
|climb rate ftmin=400
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=1.4
|wing loading note=
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|more performance=
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}}{{aircontent
|see also=
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References

1. ^¹²³Bernard, Mary and Suzanne B. Bopp: Summit Aerosports: Summit 2, Steel Breeze and Mini Breeze, Kitplanes, Volume 29, Number 12, December 2012, pages 27-28. Belvoir Publications. ISSN 0891-1851
2. ^¹²{{cite web|url = http://www.steelbreezeppc.com/mini-breeze.htm|title = 103 Mini Breeze|accessdate = 27 November 2012|last = Summit Aerosports|year = 2012}}

External links

3 : United States ultralight aircraft 2000–2009|Single-engined pusher aircraft|Powered parachutes