Schreder HP-18

Schreder HP-18

__NOTOC__ Infobox Aircraft
name=HP-18


caption=
type=Club (formerly 15 metre) class Sailplane
manufacturer=Homebuilt
designer=Richard Schreder
first flight=
introduced=
retired=
status=
primary user=
more users=
produced=
number built=
variants with their own articles=

The HP-18 is a Richard Schreder-designed metal Racing Class sailplane that was offered as a kit for homebuilding during the 1970s and 1980s. cite web|url = http://www.sailplanedirectory.com/PlaneDetails.cfm?PlaneID=165 |title = HP-18 HP Aircraft, LLC |accessdate = 2008-07-24|last = Activate Media|authorlink = |year = 2006]

Description

The HP-18 is a flapped (15-meter) sailplane featuring a V-tail and 90-degree flaps for glidepath control. The fuselage is composed of a prefabricated composite forward fuselage and a semi-monocoque aft fuselage, and features steeply reclined seating and a side-stick controller although modifications using a conventional stick have been made.

Major features:
*Very low cockpit with reclining seating position
*Sidestick (changed to conventional stick by some homebuilders)
*Two-piece canopy (changed to single piece forward opening by some homebuilders)
*V-tail that folds upwards for easy storage
*Wing structure composed of spars with caps pre-machined from solid aluminium plate and aluminium wing skins bonded to closely spaced foam ribs
*Fiberglass fuselage pod, wing tip skids and tail fairings
*Aluminium tail cone
*Winglets added by some homebuilders
*Water ballast carried inside the hollow aluminium wing spars
*Typical Schreder trailing edge flaps/airbrakes partially interconnected with the ailerons

Variants

As most homebuilts, the HP-18 has been constructed with many variations in detail. Perhaps the most significant version is the Super HP-18 developed by Canadians Ed Hollestelle and Udo Rumpf, which features a modified wing airfoil, winglets, a front-hinged canopy, conventional control stick and higher ballast capacity.

pecifications

aerospecs
met or eng?= eng

crew=One pilot
capacity=
length m=7.07
length ft=23
length in=2.4
span m=15.00
span ft=49
span in=2
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=
height ft=
height in=
wing area sqm=10.5
wing area sqft=113
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio= 21.4
empty weight kg=213
empty weight lb=470
gross weight kg=446
gross weight lb=970
lift kg=
lift lb=

eng1 number=
eng1 type=
eng1 kw=
eng1 hp=
eng1 kn=
eng1 lbf=
eng1 kn-ab=
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eng2 number=
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max speed kmh=240
max speed mph=150
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio= 38
climb rate ms=
climb rate ftmin=
sink rate ms= 0.6
sink rate ftmin= 126

armament1=
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aircontent
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References

* [http://www.soaridaho.com/Schreder/ Schreder Designs webpage]
*R Johnson, "A Flight Test Evaluation of the HP-18W Sailplane", Soaring, July 2003

External links

* [http://www.soaridaho.com/Schreder/HP-18/HP-18_Soaring_Review.html HP-18 Reference Info Link]


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