Stargate YT-33

{{Short description|American homebuilt aircraft}}

{{Merge to|Windstar YF-80|date=May 2025|reason=Not a different aicraft, different subject. It's the exact same prototype plane, simply with a different engine put in it.|talk=Talk:Windstar YF-80#Merge from Stargate YT-33}}

{{Use mdy dates|date=January 2022}}

{{Use American English|date=January 2022}}

{{Infobox aircraft begin

|name = YT-33

|image =

|caption =

}}

{{Infobox aircraft type

|type = Homebuilt aircraft

|national origin = United States

|manufacturer = Stargate, Inc.

|designer =

|first flight =

|introduced =

|retired = 2018

|status = Production completed (1994)

|primary user =

|more users =

|produced =

|number built = One

|developed from = Lockheed T-33
Windstar YF-80

|variants with their own articles =

}}

The Stargate YT-33 is an American homebuilt aircraft that was designed and intended to be produced by Stargate, Inc., of McMinnville, Oregon. It was introduced in 1994. The aircraft is a 2/3 scale replica of the Lockheed T-33 jet trainer.{{cite book |last=Purdy |first=Don |title=AeroCrafter: Homebuilt Aircraft Sourcebook |edition=5th |publisher=BAI Communications |date=July 15, 1998 |isbn=0-9636409-4-1 |page=359}}

Listed as "under development" in 1998, the YT-33 was planned to be supplied as a kit for amateur construction, but it is unlikely any kits were ever shipped.

Design and development

The YT-33 features a cantilever low wing, a two-seats-in-tandem enclosed cockpit under a bubble canopy, retractable tricycle landing gear, and a single jet engine.

The aircraft is made from composite material. Its {{convert|26.67|ft|m|1|abbr=on}} span wing has a wing area of {{convert|110.0|sqft|m2|abbr=on}}. The prototype uses a {{convert|880|lbf|kN|abbr=on}} thrust Turbomeca Marboré IIC jet powerplant.{{cite web |title=N-Number Inquiry Results - N91SH |publisher=Federal Aviation Administration |date=22 July 2022 |url= https://registry.faa.gov/aircraftinquiry/Search/NNumberInquiry |access-date=July 22, 2022}}

The aircraft has a typical empty weight of {{convert|2205|lb|kg|abbr=on}} and a gross weight of {{convert|2920|lb|kg|abbr=on}}, giving a useful load of {{convert|715|lb|kg|abbr=on}}. The aircraft has a fuel capacity of {{convert|200|u.s.gal}} or {{convert|1358|lb|kg|abbr=on}} of Jet-A.

The ISA standard temperature, sea-level, no-wind, take-off distance is {{convert|2000|ft|m|0|abbr=on}}, and the landing roll is {{convert|3000|ft|m|0|abbr=on}}.

The manufacturer estimated the construction time from the proposed kit to be 3000 hours.

Operational history

By 1998, the company reported that one aircraft had been completed and was flying.

On April 18, 2018 the one example that had been registered in the United States with the Federal Aviation Administration was de-registered; the aircraft may not exist any longer.

Specifications (YT-33)

{{Aircraft specs

|ref=AeroCrafter

|prime units?=imp

|genhide=

|crew=one

|capacity=one passenger

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|length ft=25

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|span ft=26

|span in=8

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|wing area sqft=110.0

|wing area note=

|aspect ratio=6.6:1

|airfoil=

|empty weight kg=

|empty weight lb=2205

|empty weight note=

|gross weight kg=

|gross weight lb=2920

|gross weight note=

|fuel capacity={{convert|200|u.s.gal}}

|more general=

|eng1 number=1

|eng1 name=Turbomeca Marboré IIC

|eng1 type=jet aircraft engine

|eng1 kn=

|eng1 lbf=880

|perfhide=

|max speed kmh=

|max speed mph=325

|max speed kts=

|max speed note=

|cruise speed kmh=

|cruise speed mph=300

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=75

|stall speed kts=

|stall speed note=

|never exceed speed kmh=

|never exceed speed mph=

|never exceed speed kts=

|never exceed speed note=

|range km=

|range miles=1200

|range nmi=

|range note=

|endurance=

|ceiling m=

|ceiling ft=30000

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=1500

|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=

|wing loading note=

|power/mass=

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}}

References

{{reflist}}