J u m p t o c o n t e n t
M a i n m e n u
M a i n m e n u
N a v i g a t i o n
● M a i n p a g e ● C o n t e n t s ● C u r r e n t e v e n t s ● R a n d o m a r t i c l e ● A b o u t W i k i p e d i a ● C o n t a c t u s ● D o n a t e
C o n t r i b u t e
● H e l p ● L e a r n t o e d i t ● C o m m u n i t y p o r t a l ● R e c e n t c h a n g e s ● U p l o a d f i l e
S e a r c h
Search
A p p e a r a n c e
● C r e a t e a c c o u n t ● L o g i n
P e r s o n a l t o o l s
● C r e a t e a c c o u n t ● L o g i n
P a g e s f o r l o g g e d o u t e d i t o r s l e a r n m o r e ● C o n t r i b u t i o n s ● T a l k
( T o p )
1 D e s i g n a n d d e v e l o p m e n t
2 V a r i a n t s
3 S p e c i f i c a t i o n s ( G H - 4 )
4 S e e a l s o
5 R e f e r e n c e s
T o g g l e t h e t a b l e o f c o n t e n t s
G r u d i e a i r e G H - 4
A d d l a n g u a g e s
A d d l i n k s
● A r t i c l e ● T a l k
E n g l i s h
● R e a d ● E d i t ● V i e w h i s t o r y
T o o l s
T o o l s
A c t i o n s
● R e a d ● E d i t ● V i e w h i s t o r y
G e n e r a l
● W h a t l i n k s h e r e ● R e l a t e d c h a n g e s ● U p l o a d f i l e ● S p e c i a l p a g e s ● P e r m a n e n t l i n k ● P a g e i n f o r m a t i o n ● C i t e t h i s p a g e ● G e t s h o r t e n e d U R L ● D o w n l o a d Q R c o d e ● W i k i d a t a i t e m
P r i n t / e x p o r t
● D o w n l o a d a s P D F ● P r i n t a b l e v e r s i o n
A p p e a r a n c e
F r o m W i k i p e d i a , t h e f r e e e n c y c l o p e d i a
The Grudieaire GH-4 is an American autogyro that was designed for homebuilt construction .
Design and development
[ edit ]
The GH-4 is a single seat autogyro constructed of welded steel tubing with aircraft fabric covering . The GH-4 uses Timken roller bearings and spruce wood core rotor blades with composite covering.[1]
Variants
[ edit ]
Grudieaire GH-4
Homebuilt
Vortech B20
[ edit ]
Data from Air Progress
General characteristics
Crew: 1
Length: 10 ft 2 in (3.10 m )
Height: 7 ft 1 in (2.16 m )
Empty weight: 240 lb (109 kg )
Gross weight: 450 lb (204 kg )
Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal)
Main rotor diameter: × 20 ft 4 in (6.20 m )
Performance
Maximum speed: 65 kn (75 mph, 121 km/h)
Cruise speed: 48 kn (55 mph, 89 km/h)
Range: 61 nmi (70 mi, 110 km )
Rate of climb: 1,650 ft/min (8.4 m/s)
See also
[ edit ]
Aircraft of comparable role, configuration, and era
References
[ edit ]
^ Air Progress Sport Aircraft : 78. Winter 1969.
R e t r i e v e d f r o m " https://en.wikipedia.org/w/index.php?title=Grudieaire_GH-4&oldid=1066518435 " C a t e g o r i e s : ● H o m e b u i l t a i r c r a f t ● A u t o g y r o s H i d d e n c a t e g o r i e s : ● C S 1 e r r o r s : m i s s i n g t i t l e ● A r t i c l e s w i t h s h o r t d e s c r i p t i o n ● S h o r t d e s c r i p t i o n w i t h e m p t y W i k i d a t a d e s c r i p t i o n
● T h i s p a g e w a s l a s t e d i t e d o n 1 8 J a n u a r y 2 0 2 2 , a t 1 9 : 0 7 ( U T C ) . ● T e x t i s a v a i l a b l e u n d e r t h e C r e a t i v e C o m m o n s A t t r i b u t i o n - S h a r e A l i k e L i c e n s e 4 . 0 ;
a d d i t i o n a l t e r m s m a y a p p l y . B y u s i n g t h i s s i t e , y o u a g r e e t o t h e T e r m s o f U s e a n d P r i v a c y P o l i c y . W i k i p e d i a ® i s a r e g i s t e r e d t r a d e m a r k o f t h e W i k i m e d i a F o u n d a t i o n , I n c . , a n o n - p r o f i t o r g a n i z a t i o n . ● P r i v a c y p o l i c y ● A b o u t W i k i p e d i a ● D i s c l a i m e r s ● C o n t a c t W i k i p e d i a ● C o d e o f C o n d u c t ● D e v e l o p e r s ● S t a t i s t i c s ● C o o k i e s t a t e m e n t ● M o b i l e v i e w
