Firebird 2001 Fire Fighting Management Support System

(IFFN No. 17 - July 1997)


Every year, forest fires bring destruction, injury, and even death. The ability of forest fire incident managers to control fires quickly, thereby limiting the damage, is to a great extent dependent on their ability to gather information, to deploy resources, and to perform emergency evacuations efficiently.

The MALAT Division of Israel Aircraft Industries, using mature Remotely Operated Air Vehicle (ROA) (or Unmanned Air Vehicle [UAV]) technology, has developed the application described herein, which provides real-time information to fire management, greatly enhancing the ability to manage resources. The application also provide fire fighters alerts, emergency communications relay, and other features beneficial for improvement of cost effective and safe fire suppression.

Needs

Fire management decisions rely primarily on fire scenario information. Several factors serve to limit the ability of the incident manager to gain relevant information:

Furthermore, the safety and well being of all fire suppression resources on the fire line, as well as their ability to effectively battle the fire, depend on radio communications, contact with immediate supervisors, knowledge of their actual location on the fire line, and prediction of fire behavior. Using the currently available resources, radio communications are sometimes of poor quality, the contact with supervisors is hindered, knowledge of location is sometimes outdated, and the means to accurately predict fire behavior are limited.

Capabilities

The system which has been successfully demonstrated in Missoula, Montana, U.S.A., in October 1996, and is capable of the following: 

 

 

118242 Byte

Fig.1. The Firebird 2001 during test flights in 1996

 

Prototype Capabilities and Features

The Civilian ROA/UAV System is structured to accept any of IAI/MALAT's airborne platforms. Nevertheless, the two platforms especially suitable for civil applications and budgets are: 

 Both configurations share the same avionics, briefly described below.

The FIREBIRD 2001 (Compact) configuration: 

 

Engine D.H. 290, 23.5 HP
Take Off Weight 140-150 kg
Pay load weight 15-25 kg
Fuel 19 kg
Loiter endurance 5 hours
Ceiling 15,000 ft
Cruise speed 60 kts

 

The Heron (Long-range, long-endurance, heavy payload) Configuration: 100 flight hours, 15 flights, including 52 continuous flight hours

 

Engine Rotax 914, 100/115 HP
Take Off Weight 1100 kg
Payload weight 250 kg
Fuel 250 kg
Loiter endurance 40 hrs (with 250 kg fuel)
Ceiling 35,000 ft
Cruise speed 80 kts
Power (electric) 4 kW

 

Common to both systems, special redundancy and BIT (Built In Test) provisions will enable a reliable, safe and simple operation of the system. The avionics package developed for any particular platform configuration can very easily be implemented on another platform configuration. Consequently the descriptions herein focus on the avionics capabilities of the prototype demonstration system, rather than on any particular aspect of the platform.

Avionics Features

 Some advantages of ROA/UAV use over other existing technologies


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