Grega Aircamper

__NOTOC__ Infobox Aircraft
name=GN-1 Aircamper


caption=
type=Sports plane
national origin=United States of America
manufacturer=Homebuilt
designer=John W. Grega
first flight=avyear|1963
introduced=
retired=
status=
primary user=
more users=
produced=
number built=
variants with their own articles=The Grega GN-1 Aircamper was a light aircraft developed in the United States in the early 1960s, originally as a personal project of its designer, but later marketed in plans form for homebuilding. John W. Grega initially set out to create a modernised version of the Pietenpol Air Camper using structural components from a Piper Cub but incorporating them into a new fuselage design based on the Pietenpol original. Two wings were designed, one based on the Cub wing, and another as a modernised version of the Pietenpol wing.

pecifications (typical)

aerospecs
ref=
met or eng?= eng

crew=One pilot
capacity=1 passenger
length m=5.59
length ft=18
length in=4
span m=8.84
span ft=29
span in=0
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=1.93
height ft=6
height in=4
wing area sqm=
wing area sqft=
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=512
gross weight lb=1,129
lift kg=
lift lb=

eng1 number=1
eng1 type=Continental A65-8
eng1 kw= 49
eng1 hp= 65
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=

max speed kmh=153
max speed mph=95
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=640
range miles=400
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=3.0
climb rate ftmin=600
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
armament4=
armament5=
armament6=

aircontent
see also=
related=
similar aircraft=
lists=

References

*
*