LaunchPoint Technologies 1500W Hybrid UAV Power System

Product catalog summary

Overview: The document provides technical specifications for the LaunchPoint Technologies 1500W Hybrid UAV Power System, designed for continuous output at 8500 rpm.

Specifications:

Rated Output: 1500W continuous at 8500 rpm.
Nominal Bus Voltage: 28V DC at 8500 rpm.
Engine Fuel: 40:1 premix.
Engine Displacement: 35 cc.
Combustion Cycle: 2-stroke.
Engine Cooling: Air-cooled.

Fuel Consumption:

Carbureted: 815 gm/kW*hr at 1.5 kW, 8500 rpm.
EFI Estimated: 600 gm/kW*hr at 1.5 kW, 8500 rpm.

System Mass: 1906 gm (including engine, ignition, muffler, alternator, fan).

Alternator Specifications:

Efficiency: 93% at 1500W, 8500 rpm.
Cooling: Air-cooled.
Stator Temperature: 90°C at 1500W, 8500 rpm, 25°C ambient, sea level.

Electronics Specifications:

Efficiency: 95% at 1500W, 28V.
Controller Rectifier Mass: 500 gm.
Optional Starter-Alternator Drive Electronics: 350 gm.

Note: This is a preliminary data sheet and specifications are subject to change.

Catalog excerpts

LaunchPoint Technologies 1500W Hybrid UAV Power System-1

LAUNC HYBRID UAV PROPULSION SYSTEMS Rated 1500W continuous output at 8500 rpm LaunchPoint Technologies

Open the catalog to page 1

LaunchPoint Technologies

Open the catalog to page 2

All LaunchPoint Technologies, Inc. catalogs and technical brochures

LaunchPoint Technologies 45kW Gen-Set
1 Page
LaunchPoint Technologies 6000W Gen-Set
1 Page