“Sol Prymus”的意思、由来-开放百科全书

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Sol Prymus

释义

Design and development
Variants
Prymus 1 Prymus 4
Specifications (Prymus 1 M)
References

name= Prymus

image=

caption=

}}{{Infobox Aircraft Type

type=Paraglider

national origin=Brazil

manufacturer=Sol Paragliders

designer=

first flight=

introduced=

retired=

status=In production (Prymus 4, 2016)

primary user=

more users=

produced= mid-2000s - present

number built=

program cost=

unit cost= €1,831 (Prymus M, 2004)

developed from=

variants with their own articles=
}}

The Sol Prymus (English: Primus, meaning Primary) is a Brazilian single-place paraglider that was designed and produced by Sol Paragliders of Jaraguá do Sul starting in the mid-2000s. It remained in production as the Prymus 4 in 2016.^[1]^[2]

Design and development

The Prymus was designed as a beginner to intermediate glider. By 2016 the design had progressed through four generations of models, the Prymus 1, 2, 3 and 4, each improving on the last. The models are each named for their relative size.^[1]

The Prymus 4 has a top and bottom wing surface made from WTX 40 - 40 g/m2 fabric, with wing ribs made from Pro Nyl 42 g/m2 rip stop covered with poliuretano and BT technology reinforcements. The lines are 1.1, 1.5 and 2.1 mm Cousin Technora Superaram, while the risers are Fitanew 15 x 2,0 mm Flat Multi 1600kg strapping. The carabiners are Ansung Precision 4mm 800kg and the pulleys are made by SOL.^[2]

Variants

Prymus 1

Prymus 1 S

Small-sized model for lighter pilots. Its {{convert|11.40|m|ft|1|abbr=on}} span wing has a wing area of {{convert|27.43|m2|sqft|abbr=on}}, 35 cells and the aspect ratio is 4.74:1. The pilot weight range is {{convert|60|to|80|kg|lb|0|abbr=on}}. The glider model is AFNOR Standard certified.^[1]

Prymus 1 M

Mid-sized model for medium-weight pilots. Its {{convert|11.88|m|ft|1|abbr=on}} span wing has a wing area of {{convert|29.77|m2|sqft|abbr=on}}, 35 cells and the aspect ratio is 4.74:1. The pilot weight range is {{convert|75|to|95|kg|lb|0|abbr=on}}. The glider model is AFNOR Standard certified.^[1]

Prymus 1 L

Large-sized model for heavier pilots. Its {{convert|12.35|m|ft|1|abbr=on}} span wing has a wing area of {{convert|32.2|m2|sqft|abbr=on}}, 35 cells and the aspect ratio is 4.74:1. The pilot weight range is {{convert|90|to|110|kg|lb|0|abbr=on}}. The glider model is AFNOR Standard certified.^[1]

Prymus 4

Prymus 4 S

Small-sized model for lighter pilots. Its {{convert|10.99|m|ft|1|abbr=on}} span wing has a wing area of {{convert|23.41|m2|sqft|abbr=on}}, 39 cells and the aspect ratio is 5.16:1. The take-off weight range is {{convert|70|to|90|kg|lb|0|abbr=on}} and glide ratio is 8.3:1. The glider model is Deutscher Hängegleiterverband e.V. (DHV) LTF/EN A certified.^[2]

Prymus 4 M

Mid-sized model for medium-weight pilots. Its {{convert|11.6|m|ft|1|abbr=on}} span wing has a wing area of {{convert|26.05|m2|sqft|abbr=on}}, 39 cells and the aspect ratio is 5.16:1. The take-off weight range is {{convert|80|to|100|kg|lb|0|abbr=on}} and glide ratio is 8.3:1. The glider model is DHV LTF/EN A certified.^[2]

Prymus 4 L

Large-sized model for heavier pilots. Its {{convert|12.08|m|ft|1|abbr=on}} span wing has a wing area of {{convert|28.27|m2|sqft|abbr=on}}, 39 cells and the aspect ratio is 5.16:1. The take-off weight range is {{convert|85|to|110|kg|lb|0|abbr=on}} and glide ratio is 8.3:1. The glider model is DHV LTF/EN A certified.^[2]

Prymus 4 XL

Extra large-sized model for even heavier pilots. Its {{convert|12.56|m|ft|1|abbr=on}} span wing has a wing area of {{convert|30.58|m2|sqft|abbr=on}}, 39 cells and the aspect ratio is 5.16:1. The take-off weight range is {{convert|100|to|125|kg|lb|0|abbr=on}} and glide ratio is 8.3:1. The glider model is DHV LTF/EN A certified.^[2]

Specifications (Prymus 1 M)

{{Aircraft specs
|ref=Bertrand^[1]
|prime units?=met

|perfhide=
|max speed kmh=45
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|g limits=
|roll rate=
|glide ratio=
|sink rate ms=1.1
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|more performance=
}}

References

1. ^¹²³⁴⁵Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 31. Pagefast Ltd, Lancaster OK, 2003. {{ISSN|1368-485X}}
2. ^¹²³⁴⁵{{cite web|url = http://www.solparagliders.com.br/solid/prymus_four.php|title = Prymus 4|accessdate = 15 November 2016|author = Sol Paragliders|date = }}

2 : Sol Paragliders aircraft|Paragliders

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