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7 k o5 ?, q, w; i6 M6 A% xFURIA 自制式直升機, g# w: y' L6 b! u* x# k
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" p- A/ b5 ?( }$ l j) F& C$ ~' XFURIA ULTRALIGHT HELICOPTER Plans
2 F; e( N% X; r: }. T) h) [" wFuriaHelicopter Specifications
/ d+ R* D. a- K$ o) T6 ? Main Rotor Diameter :
# p; z) c. ~! h& r( x5 _) e Main Rotor Blade Chord 4 U$ z) Y7 N3 H4 v' N; i
Main Rotor Speeds: 7 S! l7 i7 w' p q: J* s+ k# N
- ?3 M& O0 Y( B/ l0 N6 |) | Tail Rotor Diameter :
+ t6 n# h1 O- G) W; w. y Tail Rotor Chord : , v0 \3 H1 x# D
Tail Rotor Speeds: 7 K: x8 |6 u$ k* G( Y# S: b7 ^' j
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Length : 7 ~( b4 Q1 l4 e0 W* H3 w0 s7 X
Height : % p) X- j9 ~5 V7 B* K
Width : " p; @* p( w d0 P
Empty Weight : " M9 J/ q! R" \
Gross Weight :
0 h) k6 I/ m+ P8 v2 o Payload ( w / full fuel ) :
1 v6 d* t# u7 E' D) b* [) \5 P
& Y3 m' F! X$ Y* ?5 j Rotax 582UL DCDI Engine : ! O! x5 {: b2 W& v
Engine Weight :
/ j3 }# ~0 T0 W |- ] GearBox out :
$ h" U* |+ ?) s K Fuel Capacity :
- U0 f% `- J y4 d7 l/ P( z- Z9 j
9 b/ I! j& H: b- w5 u6 g Performance : L# `, U: r: I
Range :
( \! G. w" G% }! C$ L( ?" Y$ E) i( E Vmax :
) I- r ?' K) E' c8 @* |2 r( {5 M Cruise speed :
# x3 b0 d: g0 M0 e( h6 x Climb rate (msl) :
+ S( H6 [" l4 S Service Ceiling :
( t# {1 u/ E0 u9 M: K Hover in ground effect: 5 u1 U2 I4 s2 F& |" X; k" X
Hover out of ground effect: Z# ~4 m' o! ~" U- u2 X9 R
Max. Endurance
* K' N! W! F! A) Z ) q) f& i% d/ I3 D1 X7 j0 ?
Design Load Factor :
6 l0 D& T' d& D2 c0 r 5 l- X. ?; w0 o" Q8 z
Seats : `4 h# u* t! c8 i; X
Price: 18’500.00$
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( z9 r. G: j" ?6 }8 R Complete set of plans with incredible clarity! (as required by FAA Part 103, Ultralight Regulations)
6 a' V1 z. l Q The FAA has ruled that the maximum speed of 63 mph normally applied to fixed wing ultralights does not apply to helicopters due to their unique power curve.
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