- Development
- Variants
- Specifications (Kaminskas Jungster I)
- See also
- Notes
- References
- External links
| name=Kaminskas Jungster I | image= | caption= }}{{Infobox Aircraft Type | type=Homebuilt aircraft | national origin=United States | manufacturer= | designer=Rim Kaminskas | first flight=1962 | introduced= | retired= | status= | primary user= | more users= | produced= | number built= | program cost= | unit cost= | developed from= | variants with their own articles=Kaminskas Jungster II
}} |
The Kaminskas Jungster I aka Papoose RK-1 Jungmeister I is a single-seat homebuilt biplane.[1] DevelopmentThe Jungster I is a single-engine, single-seat biplane with conventional landing gear. It was intended to be an 80 percent scale replica of the Bücker Bü 133 for homebuilt construction. The wings are swept back an additional two degrees from the Jungmeister. The fuselage uses wood trusses and the wings use spruce wood spars with fabric covering.[2][3] Rights to the Jungster I were sold to Kate & Stan McLeod (K & S). Variants- Kaminskas Jungster II
- A parasol version based on the Jungster I
Specifications (Kaminskas Jungster I) {{Aircraft specs
|ref=Jane's All the World's Aircraft 1967–68[4]
|prime units?=kts
|genhide=
|crew=one
|capacity=
|length m=
|length ft=16
|length in=0
|length note=
|span m=
|span ft=16
|span in=8
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=80
|wing area note=
|aspect ratio=6.25:1
|airfoil=NACA 4413
|empty weight kg=
|empty weight lb=606
|empty weight note=
|gross weight kg=
|gross weight lb=850
|gross weight note=(aerobatic)
|max takeoff weight kg=
|max takeoff weight lb=1000
|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=
|lift note=
|more general=
|eng1 number=1
|eng1 name=Lycoming O-235-C
|eng1 type=air-cooled four-cylinder horizontally-opposed piston
|eng1 kw=
|eng1 hp=100
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|prop blade number=2
|prop name=McCauley fixed pitch
|prop dia m=
|prop dia ft=5
|prop dia in=8
|prop dia note=
|perfhide=
|max speed kmh=
|max speed mph=130
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=
|cruise speed mph=120
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=50
|stall speed kts=
|stall speed note=
|range km=
|range miles=200
|range nmi=
|range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=
|ceiling ft=13000
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=1500
|climb rate note=
|time to altitude=
|more performance=
|avionics=
}}
See also{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}Notes1. ^{{cite journal|magazine=Air Trails|date=Winter 1971|page=79}}
2. ^{{cite journal|magazine=Sport Aviation|date=February 1965|page=10|title=The Papoose RK-1 Jungmeister I}}
3. ^{{cite journal|magazine=Air Progress Sport Aircraft|date=Winter 1969|page=45}}
4. ^{{Harvnb|Taylor|1967|p=279}}
References- {{cite book |last=Taylor |first=John W. R. |authorlink=John W. R. Taylor |title=Jane's All The World's Aircraft 1967–68 |year=1967 |publisher=Sampson Low, Marston & Company |location=London |ref=harv}}
External links- [https://sites.google.com/site/jungsterbipe/jungster1biplaneinfo Jungster I]
1 : Homebuilt aircraft |