ARMSNET
Military Equipment Database
Initializing 0%

Camcopter S-100

Camcopter S-100

Reconnaissance Rotorcrafts
Spotted an error? Sign in to suggest an edit.
Basic Information
Name
Camcopter S-100
Designation
Camcopter S-100
Alternate Designation
Equipment Type
Reconnaissance Rotorcrafts
Manufacturer
Schiebel
Date of Introduction
2014
Description

The Camcopter S-100 is a highly versatile, carbon-fiber monocoque, unmanned rotorcraft being developed by Schiebel to meet the requirements of military and civil customers using a variety of modular payloads. As a vertical take-off and landing (VTOL) air vehicle the S-100 eliminates the need for launch and recovery equipment. The air vehicle can be programmed to fly an autonomous mission profile relying on its GPS/INS navigation system. Schiebel has provided the S-100 with integrated checklists and numerous fail-safe mechanisms to reduce the risk of damage due to operator error. A built-in two-way datalink enables to receive control inputs and to send video and imagery to the ground control station in real time. Schiebel is targeting the S-100 rotorcraft for both ground- and ship-based applications such as tactical surveillance and reconnaissance, artillery support, maritime surveillance and amphibious support, and weapons delivery. The Camcopter S-100 has two payload bays, side hard points and an internal auxiliary electronics/avionics bay. The primary payload bay, located directly beneath the main rotor shaft, is capable of mounting payloads weighing up to 50 kg (100-lb). Typically, the payload consists of daylight TV and/or infrared cameras. Besides, the S-100 could conduct precise delivery and recovery of guided munitions, deployment of riot control agents (smoke), and mine detection using infrared camera. The air vehicle is powered by a 55-hp aviation engine which provides a maximum speed of 120-kt and a flight endurance of up to six hours carrying a 34 kg payload and cruising at 55 knots. The mission range varies from 80 to 130 kilometers.

Air & Air Defense Specifications
Max Speed 222.2 km/h
Range 130.0 km
Service Ceiling 5486 m
Overview (Deagel)
Group Reconnaissance Rotorcrafts
Status Active
Origin Austria
Contractor Schiebel
Initial Operational Capability (IOC) 2014
Total Production ?
Specifications (Deagel)
Main Rotor Blades 2
Dimensions — Height 1,120 millimeter
Dimensions — Length 3,110 millimeter
Dimensions — Main Rotor Diameter 3,400 millimeter
Dimensions — Width 1,240 millimeter
Mass — Empty Weight 97 kilogram
Mass — Max Takeoff Weight 200 kilogram
Mass — Payload 50 kilogram
Performance — Ceiling 18,000 foot
Performance — Max Range 130 kilometer
Power — Max Power at TakeOff 55 hp
Speed — Cruise Speed 55 knot
Speed — Top Speed at High Altitude 120 knot
Time — Flight Endurance 6 hour
Gear (Deagel)
Item 1 Mapping Systems: PicoSAR (1)
Details
Country of Origin Austria
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
3.11 m
Width
1.24 m
Height
Weight
200 kg
Operators (3)
Russia
Austria
Myanmar
Something went wrong. Please reload the page. Reload