Windward Performance SparrowHawk

{{Infobox aircraft begin

| name=SparrowHawk

| image=Windward Performance SparrowHawk 2-view.svg

| caption=Three view drawing

}}{{Infobox aircraft type

| type=Glider

| national origin=United States

| manufacturer=Windward Performance

| designer=

| first flight=2002

| introduced=

| retired=

| status=Out of Production

| primary user=

| more users=

| produced=

| number built=35

| program cost=

| unit cost= US$44,500.00 (2011){{Cite web|url = http://www.windward-performance.com/pricing.php|title = Pricing and Options|accessdate = 26 October 2011|last = Windward Performance|authorlink = |date=February 2011}}

| developed from=

| variants with their own articles=

}}

The Windward Performance SparrowHawk is an American mid-wing, single-seat glider that was designed and produced by Windward Performance.Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 60. Pagefast Ltd, Lancaster OK, 2003. {{ISSN|1368-485X}} It first flew in 2002.{{Cite web |title=J2mcL Planeurs - Fiche planeur n° |url=https://www.j2mcl-planeurs.net/dbj2mcl/planeurs-machines/planeur-fiche_0int.php?code=2457 |access-date=2022-05-21 |website=www.j2mcl-planeurs.net}}

Since 2016 the aircraft has been no longer advertised as available by the manufacturer.{{cite web|url = http://windward-performance.com/|title = Windward Performance home page|accessdate = 1 December 2016|author = Windward Performance|year = 2016}}

Design and development

The SparrowHawk was designed to fit into the US FAR 103 Ultralight Vehicles category, including that category's requirement that unpowered aircraft have a maximum empty weight of {{convert|155|lb|kg|0|abbr=on}}. The sailplane achieves this by utilizing a structure that is predominantly made from carbon-fiber-reinforced polymer.{{Cite web|url = http://www.windward-performance.com/faq.php|title = Frequently Asked Questions|accessdate = 26 October 2011|last = Windward Performance|authorlink = |date=February 2011|archiveurl = https://web.archive.org/web/20111118185125/http://www.windward-performance.com/faq.php |archivedate = 18 November 2011}}

The SparrowHawk's multi-tapered, {{convert|36.1|ft|m|1|abbr=on}} span wing employs five different airfoils and has an aspect ratio of 18.6:1. The wing features Schempp-Hirth style spoilers on the top surface. The cockpit can accommodate pilots who range in height from {{convert|63|to|75|in|cm|0|abbr=on}}. The landing gear is a fixed monowheel gear with an auxiliary tail wheel. The glider is finished with a two part polyurethane paint. The aircraft can be launched by auto-tow, winch-launch, or aero-tow by both light aircraft and ultralight aircraft. Aerobatics are not recommended.

The SparrowHawk achieves a best glide ratio of 36:1 and a minimum sink rate of 119 ft/min (0.60 m/s).{{Cite web|url = http://www.windward-performance.com/specifications.php|title = SparrowHawk Specifications and Performance|accessdate = 26 October 2011|last = Windward Performance|authorlink = |date=February 2011|archiveurl = https://web.archive.org/web/20111117221808/http://www.windward-performance.com/specifications.php |archivedate = 17 November 2011}}

Specifications (SparrowHawk)

{{Aircraft specs

|ref=Bertrand and company website

|prime units?=kts

|genhide=

|crew=one

|capacity=

|length m=

|length ft=20.6

|length in=

|length note=

|span m=

|span ft=36.1

|span in=

|span note=

|height m=

|height ft=4.5

|height in=

|height note=

|wing area sqm=

|wing area sqft=70

|wing area note=

|aspect ratio=18.6:1

|airfoil=

|empty weight kg=

|empty weight lb=155

|empty weight note=

|gross weight kg=

|gross weight lb=415

|gross weight note=

|more general=

|perfhide=

|max speed kmh=

|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=32

|stall speed note=

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=123

|never exceed speed note=

|g limits=+5.48/-4.0g

|roll rate=

|glide ratio=36:1 at 50 kn (58 mph; 93 km/h)

|sink rate ms=

|sink rate ftmin=119

|sink rate note=at 38 kn (44 mph; 70 km/h)

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=5.93

|wing loading note=

|more performance=

|avionics=

}}

See also

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References

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