Giravia: LP-10

General data

Producer info

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Names and dates
Market original model designation
LP-10
Market model designation (english translation or spelling)
LP-10
Date of prototype completion
1952
Tests start date
1954-04-14
Country of manufacture
France
People involved
M. PouitFunction unknown
Lepere {Lepère}Function unknown
Config info
Rotorcraft typeHelicopter
Config
Single rotor
Way of counteracting main rotor torque
Counteracting torque not required
Weights
Manufacturers empty weight (MEW)
400
kg
Cabin and cockpit
Maximum number of people onboard
2
Cockpit seating arrangement
Side-by-side
Cabin type
Enclosed
External dimensions
Landing gear type
Skids
Main rotor
Main rotor equipped with stabilizing bar
No
Main rotor equipped with servo-rotor
Yes
Drive type
Tip jets
Main rotor diameter
12
m
Main rotor direction of rotation
Counterclockwise
Number of blades
2
Powerplant
Engine model
Turboméca Aspin III
Engine model (english translation or spelling)
Turbomeca Aspin III
Engine type
Turbojet
Number of engines
1
Performance
Maximum horizontal flight speed (Vh)
140
km/h
0.0514