Aircraft Overview

FLM 136 is a reliable, cost effective, group 3 threat emulator with an open architecture. It is available in a target or threat configuration, and has the option of pneumatic catapult, rocket assisted takeoff (RATO), or truck launch. The crew consists of the operator, safety pilot, and ground personnel.

Dedicated payload bays and a removable nose cone combine to provide a 40 lb payload capacity, making the aircraft flexible to perform various tasks.

The air frame is manufactured using lightweight carbon fiber and composite materials to achieve an optimal strength to weight ratio. The airframe and subcomponents have been tested successfully to withstand stress witnessed in normal flight conditions while retaining an ample safety margin. The main components of the airframe consist of the fuselage, wings, and nose cone.

Sapphire UAS

Aircraft Specs

Parameter Specification
Length 9.8 ft
Wingspan 8.2 ft
Engine DA 215 carbureted
Empty Weight 78.5 lbs
Fuel Capacity 72.6 lbs (12.1 gal)
Payload Capacity 40 lbs
Max Gross Takeoff Weight (MGTOW) 180 lbs
Construction Carbon fiber
Endurance 6 hours
Cruise Airspeed 74 kts
Max Airspeed 105 kts
Takeoff Truck Launch, RATO, Pneumatic Catapult
Landing Belly

Engine

The FLM136 uses a high performance carbureted, two-stroke internal combustion engine mounted at the rear of the fuselage in a pusher configuration. The engine assembly includes all electronics, RPM sensor, ignition module, vibration mount, and propeller. Fuel is held in an integral composite tank located within the fuselage. The tank is equipped with anti-slosh baffles and an internal fuel filter.

Engine Specs

Parameter Specification
Engine Carbureted two-stroke
Weight 10.9 lbs
Displacement 13.12 ci / 215 cc
RPM Range 2,500 - 6,700 RPM
Fuel Type 91-93 octane, C10
Oil Red Line Two-Stroke Racing Oil
Fuel Consumption ~12 lbs/hr (2 gal/hr)
Fuel Capacity 72.6 lbs (12.1 gal)
Propeller 23x10

results matching ""

    No results matching ""