Шевко С. В.: Триумф
Shevko S. V.: Triumph

General data

Producer info

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Names and dates
Market original model designation
Триумф
Market model designation (english translation or spelling)
Triumph
Project start date
1998
Country of manufacture
Ukraine
People involved
Sergey Shevko {Сергей Шевко}Constructor
Config info
Rotorcraft typeAutogyro
Weights
Maximum Takeoff Weight (MTOW)
160
kg
Manufacturers empty weight (MEW)
65
kg
Cabin and cockpit
Maximum number of people onboard
1
External dimensions
Height
2.10
m
Main rotor
Main rotor type
Semi-rigit
Cyclic control
Tilting rotor shaft
Collective control
Yes
Main rotor diameter
7
m
Prerotation
Yes
Prerotation type
Mechanical
Number of blades
2
Minimum collective pitch angle
0
°
Maximum collective pitch angle
12
°
Main rotor blade chord
0.28
m
Main rotor blade airfoil
NACA 8-H-12
Main rotor blade twist
0
°
Propeller
Mode
Pushing
Propeller diameter
1.60
m
Propeller pitch mode
Adjustable on the ground
Number of blades
2
Propeller material
Wood
Powerplant
Engine model
Simonini
Engine model (english translation or spelling)
Simonini
Engine type
Piston
Number of engines
1
Total maximum power
28
HP
Performance
Maximum horizontal flight speed (Vh)
120
km/h
Best range speed (Vbr)
80
km/h
Best rate of climb
4
m/s
Miminum rate of descend in autorotation
6
m/s
Maximum service ceiling
3500
m
Jump take-off availability
Yes
Heigh achieved during jump take-off
28
m
(...)
25
m
Best glide ratio
6
Maximum range
300
km
0.1195