Air Force Technology
Dimensions:
Wingspan28.50m / Length29.39m / Height7.87m
Engines:Type2 × Rolls-Royce BR710C4-11 turbofan engines / Engine Power 68.4kN
Performance:Maximum Speed (Mmo) Mach 0.885 / Endurance: 9 hours at mission radius of 185km, altitude 12,500m
Range at Mach 0.8012,501km
Mission Systems:Mission Stations6 × multi-purpose operator stations
CAEW and Control System / EL/W-2085EL/W-2085 Radar1-2 GHz and 2- 4GHz
Satellite CommunicationsEL/K-1891Satcoms Frequency BandKu band, 12.5GHz-18GHz
The Israel Aerospace Industries (IAI) conformal airborne early warning and control (CAEW) aircraft was first unveiled in public at the UK’s 2008 Farnborough Air Show. The prime contractor, system developer and system integrator for the CAEW is Elta Systems Ltd, a subsidiary of IAI.
The CAEW aircraft is based on the G550 airframe from Gulfstream Aerospace of the USA. The operationally proven G550 CAEW aircraft is the third generation of airborne early warning and control systems developed by IAI Elta since the mid-1980s.

Gulfstream was awarded a contract for four (plus two options) G550 modified aircraft in August 2003. First flight of the modified aircraft was in May 2006 and it was delivered to Elta for the installation of the mission systems in September 2006. The first and second CAEW aircraft were delivered to the Israel Air Force in February and May 2008 and since then have been in operational use.
The Singapore Air Force has also ordered a number of CAEW aircraft to be delivered during 2009 and 2010.

The CAEW provides improved performance in terms of higher operating altitude, longer range and increased time on station. The main AEW performance advantages result from the capability to point the radar beams in any direction in space at any time, with the beam’s parameters controlled by the radar computer.
CAEW airframe
The CAEW aircraft is based on the Gulfstream G550 airframe, which is an upgraded variant of the Gulfstream V-SP with improved aerodynamic performance. The aircraft is manufactured at the Gulfstream business jet production centre in Savannah, Georgia, USA and transferred to IAI Elta Systems Ltd in Ashdod, Israel.
Compared to the original G550, the CAEW redesigned aircraft has an increased zero-fuel weight, a modified structure, additional cabling, three (instead of one) power generators and a liquid cooling system to accommodate the mission equipment. One particular specification is the aircraft’s low drag aerodynamic profile.
IAI’s Bedek Aviation is contracted to provide the maintenance and logistic support for the Israeli CAEW aircraft.
Cockpit
The baseline G550 aircraft uses a Honeywell Primus Epic avionics suite and the two-man flight deck has a Gulfstream PlaneView cockpit. The CAEW flight deck provides the pilot with real-time 360°, three-dimensional AEW information.
Mission systems
The AEW system has six multi-purpose, Windows-based, operator stations with 24in colour monitors that are installed in the rear half of the main cabin. The forward section of the main cabin behind the cockpit accommodates the electronics.

The Elta AEW system provides rapid target acquisition and target information with total 360° coverage. Avoiding host aircraft obstruction is achieved by using the placement of a number of conformal antennae combined with dynamic beam allocation to the targets. The multiple conformal antennae provide the coverage without the need for a large mushroom-shaped radar system installed on comparable aircraft.
The aircraft is equipped with the Elta EL/W-2085 AEW system which includes a phased array airborne early warning radar, an identification friend or foe system, electronic support measures (ESM), electronic intelligence (ELINT) and communications intelligence (COMINT) systems.
The system is highly automated and uses advanced multi-sensor data fusion techniques to cross-correlate data generated by all four sensors - the radar, IFF, ESM / ELINT and CSM / COMINT. The data is combined with an automatically initiated active search by one sensor for specific targets that have been detected by other sensors.
The phased array airborne early warning radar, an active electronic steering array (AESA), operates in L and S bands (1GHz to 2GHz and 2GHz to 4GHz) and provides 360° azimuthal coverage. The system has high-accuracy three-dimensional tracking, low false-alarm rate, flexible and high target revisit time, electronic counter-countermeasures and programmable search and track modes of operation.
The modes of operation include track initiation, extended detection range mode with long dwell time, and target verification. When a target has been identified as a priority the radar switches to a high scan rate tracking mode with optimised beam to target characteristics.

The forward-facing hemisphere radar array and the weather radar are mounted in the nose radome. The lateral arrays are housed in conformal radomes along the sides of the forward fuselage. The radome located on the tailcone houses the aft facing hemispherical array.
The information friend or foe system uses the radar’s receive / transmit modules and antennae and provides target interrogation, decoding, target detection, location and target tracking.
The electronic support measures and electronic intelligence systems use multiple narrow and wideband receivers. The ESM / ELINT also provides the radar warning receiver function and supports the aircraft’s self-protection system. The antenna pods are mounted under the wingtips. An electronic support measures antenna is mounted in a fairing above the nose cone which houses the weather radar. The direction finding function uses differential time of arrival.
The automated communications intelligence system covers the high (HF) to very-high (VHF) frequency bands from 3MHz to 3GHz.
Communications
The aircraft’s communications suite provides network-centric operations capability and is interoperable with air force, navy and ground force assets and includes U/VHF, HF, satellite communications, voice over internet protocol (VoIP), secure voice, secure data link and intercom.
The aircraft is fitted with a robust jam-resistant full duplex EL/K-189 satellite communications and datalink. The satellite communications operates at Ku band, 12.5GHz to 18GHz. The satellite antenna dish and one planar array are housed in the vertical tail surface top fairing and another planar array is housed in a ventral blister radome. The antennae are dual axis stabilised with pointing capability. The carrier link can provide voice, data and compressed video.
The aircraft can be fitted with the data link specified by the customer country.
CAEW countermeasures
The aircraft is fitted with an integrated self protection suite with 360° radar warning receiver (RWR), missile approach warning system (MAWS), chaff and flare decoy dispensers and directed infrared countermeasures (DIRCM).
Engines
The aircraft is powered by two Rolls-Royce BR710C4-11 turbofan engines rated at 68.4kN and fitted with full authority digital engine control (FADEC). The engines are fitted at the rear of the fuselage. The integral wing tanks have a fuel capacity of 23,400l and the fuel system is equipped with an automatic fuel distribution system to accommodate the changing fuel load during flight.
The aircraft is equipped with a Hamilton Sundstrand electrical power generation system and the CAEW aircraft also has power generators mounted on the engines providing 240kW of power.
Gulfstream was responsible for the design and supply of the liquid cooling system to accommodate the high power consumption of the airborne electronics.
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According to Nissim Hadas, general manager of IAI’s Elta Systems, the prime contractor for the program, the new CAEW reflects the company’s advanced systems approach, based on vertically integrated system of systems, based on Elta-unique technologies and know-how developed in-house. The CAEW is a member of a family of new special mission aircraft, which also includes the AISIS airborne integrated SIGINT system and the MARS, an Airborne SAR platform. The first two are already operational with the Israel Air Force and the MARS is also part of the IAF’s long term strategy.
According to Avishai Izhakian, general manager of Elta’s AEW plant the conformal phased-array radar configuration utilized with the CAEW offers “the optimal configuration for high performance at the most affordable life cycle cost.” The aircraft can remain on station for nine hours at maximum altitude, operating at a range of about 100 nautical miles from its base. The aircraft is fitted with four AESA radar planes, two S band AESA systems are positioned in fore, aft while two sides looking L-band arrays are covering port and starboard, effectively covering 360 degrees.

According to Izhakian, the G550 AEW platform can fly higher than its competitors such as the Boeing 737 and Saab 340 or Emb145 (Erieye) platforms, furthermore, it can generate significantly more missions, since its maintenance and support procedures are shorter.
The CAEW represents the third generation of phased array airborne radar technology developed at Elta Systems. Elta entered the world of phased array radars in the 1980s, implementing the technology with the Green Pine ballistic missile warning radar (part of the Arrow ATBM system). The same technology packaged as ‘Phalcon’ AEW radar, was installed on a modified Boeing 707 dubbed ‘Condor’, developed for the Chilean air force, which became the first operator of full-size phased array AEW system. This aircraft became operational in the mid 1990s. Soon after, China ordered three similar Phalcon radars, with the radars configured on Russian Il-76 aircraft.
However, encountering fierce US objection to the deal, Israel decided to terminate the program, leaving IAI with unclear future about its AEW thrust. “Despite the significant impact of the termination of this work, we managed to keep our employees and maintain the knowledge base to be able to continue and develop a second and third generations of the phased-array AEW technology we pioneered in the 1990s. ” said Nissim Hadas. The results of this effort were realized few years later, with the signature of a contract to supply IL-76TD AEW aircraft to India, fitted with a 11 meter elevated radom, and G550 based third generation CAEW to the Israel Air Force. Both versions are being delivered this year (2008). The first two CAEW aircraft were delivered in February and May and the first Il76 is scheduled for delivery in September 08. The remaining aircraft will be supplied in 2009-2012. Earlier this year the Singaporean Ministry of Defense announced that the Singapore Air Force will also receive several CAEW aircraft in the upcoming months.
