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Introduction
 The Dassault nEUROn is an experimental Unmanned Combat Air
Vehicle (UCAV) being developed with international cooperation,
led by the French company Dassault Aviation.
 This flying wing stealth UCAV project is the final phase of the
French Dassault LOGIDUC 3-step stealth "combat drone"
programme.
 Until June 2005 it had the form of the original Dassault developed
Grand Duc vehicle: supersonic two-engined long-range
unmanned bomber, capable of performing attacks with nuclear
weapons.
Aim
 The aim of the nEUROn programme is to demonstrate the maturity and the effectiveness of
technical solutions, but not to perform military missions.
 The main technological challenges addressed during the design phase of the nEUROn are:
 The shapes of the air vehicle (aerodynamic, innovative composite structure, and internal
weapon bay),
 The technologies related to low observability issues,
 The insertion of this type of aircraft within the test area,
 The high-level algorithms necessary to the development of the automated processes,
 As well as the place of the human factor within the mission loop.
 The last, but certainly not the least, important technology to be demonstrated is the
capability to carry and deliver weapons from an internal bay.
 Today, European aircraft are designed with external loading capabilities for bombs and
missiles.
Goals
 The performance of an air-to-ground mission based on the
detection, localization, and reconnaissance of ground targets in
autonomous modes,
 The evaluation of the detection results of a stealth platform
facing ground or aerial threats, in terms of radar cross section
and infrared signature,
 The weapon release from an internal bay, with the very stringent
tempo constraints of a fast decision loop.
Platform
 As a UCAV, nEUROn will be significantly larger and more advanced than
other well-known UAV systems like the MQ-1 Predator, with ranges, payloads
and capabilities that approach those of manned fighter aircraft.
 Indeed, Saab's February 9, 2006 release notes that nEUROn will be a
demonstrator measuring 10 m long by 12 m wide and weighing in at 5 tons.
 The aircraft will have unmanned autonomous air-to-ground attack
capabilities with precision guided munitions, relying on an advanced stealth
airframe design to penetrate undetected.
 Another feature being contemplated is the ability of grouping the nEUROns
and controlling the group in a manner similar to many combat real-time
strategy computer games.
Specifications
 Crew: 0
 Length: 9.5 m (31 ft 2 in)
 Wingspan: 12.5 m (41 ft 0 in)
 Empty weight: 4900 kg (10803 lb)
 Gross weight: 7000 kg (15432 lb)
 Powerplant: 1 × Rolls-Royce/Snecma M88, 40 kN (8992 lbf) thrust each
 Maximum speed: 980 km/h (608 mph) km/h ( mph)
 Service ceiling: 14,000 m (45900 ft)
References
 http://www.aereo.jor.br/wp-content/uploads//2012/03/41547_38899.jpg
 http://www.google.co.in/url?sa=t&rct=j&q=&esrc=s&source=web&cd=1&cad=rja&uact=
8&ved=0CB0QFjAA&url=http%3A%2F%2Fen.wikipedia.org%2Fwiki%2FDassault_nEUROn&ei
=HZbWU9HLJ5D38QXw4YCADg&usg=AFQjCNEWPMbb0fDglkUc8oGuSPGZjbK1eA&bvm=
bv.71778758,d.dGc
 http://www.dassault-aviation.com/en/defense/neuron/introduction/
 http://37.media.tumblr.com/71445f5083d2bcac08b38851a8cf0951/tumblr_mfmz2t9QOJ1
s18qwwo1_1280.jpg
Neuron

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Neuron

  • 1.
  • 2. Introduction  The Dassault nEUROn is an experimental Unmanned Combat Air Vehicle (UCAV) being developed with international cooperation, led by the French company Dassault Aviation.  This flying wing stealth UCAV project is the final phase of the French Dassault LOGIDUC 3-step stealth "combat drone" programme.  Until June 2005 it had the form of the original Dassault developed Grand Duc vehicle: supersonic two-engined long-range unmanned bomber, capable of performing attacks with nuclear weapons.
  • 3.
  • 4. Aim  The aim of the nEUROn programme is to demonstrate the maturity and the effectiveness of technical solutions, but not to perform military missions.  The main technological challenges addressed during the design phase of the nEUROn are:  The shapes of the air vehicle (aerodynamic, innovative composite structure, and internal weapon bay),  The technologies related to low observability issues,  The insertion of this type of aircraft within the test area,  The high-level algorithms necessary to the development of the automated processes,  As well as the place of the human factor within the mission loop.  The last, but certainly not the least, important technology to be demonstrated is the capability to carry and deliver weapons from an internal bay.  Today, European aircraft are designed with external loading capabilities for bombs and missiles.
  • 5.
  • 6. Goals  The performance of an air-to-ground mission based on the detection, localization, and reconnaissance of ground targets in autonomous modes,  The evaluation of the detection results of a stealth platform facing ground or aerial threats, in terms of radar cross section and infrared signature,  The weapon release from an internal bay, with the very stringent tempo constraints of a fast decision loop.
  • 7.
  • 8. Platform  As a UCAV, nEUROn will be significantly larger and more advanced than other well-known UAV systems like the MQ-1 Predator, with ranges, payloads and capabilities that approach those of manned fighter aircraft.  Indeed, Saab's February 9, 2006 release notes that nEUROn will be a demonstrator measuring 10 m long by 12 m wide and weighing in at 5 tons.  The aircraft will have unmanned autonomous air-to-ground attack capabilities with precision guided munitions, relying on an advanced stealth airframe design to penetrate undetected.  Another feature being contemplated is the ability of grouping the nEUROns and controlling the group in a manner similar to many combat real-time strategy computer games.
  • 9.
  • 10. Specifications  Crew: 0  Length: 9.5 m (31 ft 2 in)  Wingspan: 12.5 m (41 ft 0 in)  Empty weight: 4900 kg (10803 lb)  Gross weight: 7000 kg (15432 lb)  Powerplant: 1 × Rolls-Royce/Snecma M88, 40 kN (8992 lbf) thrust each  Maximum speed: 980 km/h (608 mph) km/h ( mph)  Service ceiling: 14,000 m (45900 ft)
  • 11.