TASGER  Industries

Technologies for the Future

Products

U N M A N N E D    A E R I A L    V E H I C L E    ( U A V )

MANA Drone equipped with integrated systems, light weight materials, innovative design and cutting-edge manufacturing technologies feasible for commercial applications and capable of heavy-lifting in set of multiple units as carriers for containers weighing in tons.

 

E L E C T R I C A L    M A C H I N E

PARYOU Motor is engineered with optimized speed, torque, efficiency and cost ideal for e-mobility.

 

P R I V A T E    P L A N E

AIRCRAFT RV-10

SPECIFICATIONS

Exterior Dimensions

Span                      9.68 m

Length                   7.44 m

Height                    2.64 m

Wing Area             13.7 sq m

Weights

Empty Weight        740 kg

Gross Weight        1225 kg

Loadings

Wing Loading        91 kg/sq m

Power Loading      6.1 - 4.7 kg/hp

Powerplant/Systems

Engine                   260 hp

Fuel Capacity        227 liter

Capacity

Occupant              4 seat

Luggage                45 kg

PERFORMANCE*

Speed 

Top Speed                                  334 km/h

Cruise [75% @ 2438.4 m]           317 km/h

Cruise [55% @ 2438.4 m]           283 km/h

Stall Speed                                 101 km/h

Never Exceed Speed                  370 km/h

Ground Performance

Takeoff Distance                         152.4 m

Landing Distance                        198.2 m

Climb/Ceiling

Rate of Climb                              7.4 m/s

Ceiling (est)                                 6096 m

Range

Range [75% @ 2438.4 m]           1327 km

Range [55% @ 2438.4 m]           1609 km

Limitation

Max. Takeoff Weight                   1181 kg

*Measured at Gross Weight (1225 kg)

 

F L I G H T    T R A I N E R 

AIRCRAFT CH 701

SPECIFICATIONS

Exterior Dimensions

Span                      9.68 m

Length                   6.38 m

Height                    2.62 m

Wing Area             11.33 sq m

Weights

Empty Weight        263 kg

Gross Weight         500 kg

Powerplant/Systems

Engine                   100 hp

Fuel Capacity        76 liter

Capacity

Occupant              2 seat

PERFORMANCE

Speed 

Top Speed                                  152 km/h

Cruise                                         136 km/h

Stall Speed                                 48 km/h

Never Exceed Speed                  177 km/h

Ground Performance

Takeoff Distance                         15.2 m

Landing Distance                        24.4 m

Climb/Ceiling

Rate of Climb                              5.1 m/s

Ceiling (est)                                 4572 m

Range

Range                                          563 km

 

T H E    C L A S S I C S

CESSNA 150, 152, 172 SKYHAWK, 182 SKYLANE, 185 SKYWAGON, 400 CORVALIS TTx
 

I N S T R U M E N T    P A N E L    A N D    A V I O N I C S    U P G R A D E

Turnkey service from equipment selection + panel design, electrical schematic definition, procurement, wiring, fabrication, finish and installation including coordination with aviation authority for Supplemental Type Certification (STC) generally required for modifications of existing aircrafts.
 

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