History of IDT Asef
The "ASEF" UAS, developed by INTRA Defense Technologies, is a versatile unmanned aircraft system designed for use in military, civilian, and industrial sectors. It excels in all-weather and terrain conditions, making it suitable for a wide range of operations, including tactical reconnaissance, surveillance, border protection, and more. One of its standout features is its vertical take-off and landing (VTOL) capability, which combines helicopter-like qualities with simplicity and cost-effectiveness.
This UAS has a compact design with key components housed in the central hull, featuring a V-shaped rear wing. It can carry a payload of up to 26 lbs and has a maximum takeoff weight of 215 lbs. With a cruising speed of 70 miles per hour, a mission duration window of around 10 hours, and the ability to reach altitudes of 18,000 feet, it offers robust performance.
The aircraft is equipped with a lightweight live camera system that supports long-range continuous zoom. It also has autonomous capabilities, reducing the need for human intervention during take-off and landing. Additionally, the system incorporates redundant safety measures, including collision detection and avoidance functions, for enhanced reliability in its operations.
Specification
Basics
Year of Service: 2021
Origins: Saudi Arabia
Status: Active.
Crew: 0
Production: 4
Manufacturer: INTRA Defense Technologies Ltd (IDT) Saudi Arabia
Carrier: Saudi Arabia (possibly)
MTOW: 212 lbs (96kg)
Roles
Close Air Support (CAS)
Designed to operate near active ground elements with a wide range of air-to-surface weapon and ammunition options.
Special Mission: Search and Rescue (SAR)
Ability to locate and evacuate personnel from potentially hazardous or dangerous areas, such as downed pilots at sea.
Intelligence Surveillance Reconnaissance (ISR), reconnaissance
Monitor ground targets/target areas to assess surrounding threat levels, enemy strength, or enemy movement.
Unmanned
Aircraft designed (or later developed) have inherent unmanned capabilities and can fill a variety of battlefield roles.
Notable Features
Vertical Takeoff/Landing (VTOL)
The series has the tactical capability of vertical take-off and/or landing, a characteristic usually associated with helicopters.
Radar capability
Houses may house (via specialized variants) radars for searching, tracking, and attacking enemy elements.
Multi-engine
Include two or more engines to improve survivability and/or performance.
Mixing Engine
Use two or more types of propulsion systems to achieve desired performance/flying maneuvers.
Fader support
The design features a rearward push rod arrangement in contrast to the more traditional pull rod arrangement.
All Electric
The design uses an all-electric powerplant for propulsion.
Extended range performance
Ability to travel long distances using on-board fuel supplies.
Operation Lakes
Able to operate over the ocean and survive certain harsh marine environments.
Unmanned operation
The design features the ability to fly without a pilot, with actions controlled by onboard programming and/or ground operators.
Autonomous operation
The design features autonomous flight operations through artificial intelligence or onboard pre-programming.
Camera equipment
Payload supports photography devices that provide real-time still images and/or image/video results.
Main Aircraft Structure
Monoplane
Designed to use a single main wing main aircraft; this is the most popular arrangement of main aircraft.
Shoulder
The main aircraft is mounted on the upper part of the fuselage, usually on an imaginary line that intersects the pilot's shoulders.
Straight
Floor plans involve the use of simple, straight main plan elements.
Performance
Installed: The electric propulsion system drives 4 lift propellers and 1 drive propeller arranged in thrust direction.
Maximum speed: 53 km/h (86 km/h | 46 knots)
Cruising speed: 43 km/h (70 km/h | 38 knots)
Maximum speed difference: +10 km/h (+16 km/h | 9 kn)
Maximum: 18,045 feet (5,500 m | 3 km)
Area: 444 km (715 km | 1,324 nautical miles)
