Rotovia
06-01-2004, 09:10
The Rotovian Government is currently selling of much of its military technology and weapons in preparation for a large sacle upgrade. More items will be added as they are cleared for sale. All items must be cleared and have been drastically reduced.
http://www.afrotc.tcu.edu/photos/%20aircraft/f117/f117_5.jpg
Delta Class Strike Cruiser: F-17 Nighthawk
Cost: $250,000
DESIGN FEATURES:
Multi-faceted airframe designed to reflect radar energy away from originating transmitter, particularly downward-looking AEW aircraft.
Use of a highly angular type of flying wing basic design (based on relaxed stability and controlled via a quadreplex fly-by-wire control system) with a butterfly tail and elements of lifting-body vehicle design.
The concept is to refelct incoming electromagnetic energy and other radiation in all directions, except the originating emitter.
Vortexes from many sharp edges, including leading-edge of wing, designed to form co-ordinated lifting airflow pattern
wings have 67 degrees 30' sweepback, all doors and access panels have serrated edges to suppress radar reflection
boom refuelling receptacle on port side of top plate, aft of cockpit. Frontal radar cross-section estimated as 0.01 m2 (0.1 sq ft).
The F-117A also has no active radars, unlike conventional warplanes. Instead, it uses a search rada being taken by an advanced passive system based on IR sensors and that of the Doppler navigation system by high-quality INS.
The F-117A also has internal accommodation for small warload of "smart" weapons, thus also reduces the aircrafts radar signature, with the absence of protruding hardpoints.
POWER PLANT:
Two 48.0 kN (10,800 lb st) class General Electric F404-GE-F1D2 dry thrust non-augmented turbofans.
Rectangular overwing air intakes with heated grid for anti-icing and low observability.
Auxiliary air intake doors in horizontal surface immediately to the rear.
Part of cold air ingested bypasses engine and is mixed with exhaust gases for cooling.
Narrow-slot 'platypus' exhausts, designed by Astech/MCI, in rear fuselage, with extended lower lip, surrounded by heat tiles of type used on Space Shuttle and with 11 vertical, internal guide vanes.
In-flight refuelling receptacle in decking aft of cockpit. Optional drop tank on internal weapons pylon.
ARMAMENT:
Full range of USAF tactical fighter ordnance, principally two 2000 lb bombs:
BLU-109B low-level laser-guided or GBU-10/GBU-27 laser-guided glide weapons
Alternatively, AGM-65 Maverick or AGM-88 HARM ASMs.
Provision for AIM-9 Sidewinder (against AWACS aircraft).
Internal carriage on two extendible beams in weapon bay. (Only missiles with seeker heads extended below aircraft prior to launch; bombs released from within weapons bay.)
http://www.capitolsource.net/%20images/prog/b2.jpg
Alpha Class Bomber Plane: B2
Cost: $450,000
DESIGN FEATURES:
The whole aircraft is the design of the relaxed-stability type, a flying wing with straight leading-edges swept at 40° with a W-shaped trailing edges.
Emphasis was placed on smooth surfaces with blended flight deck and nacelle bulges.
Use of radiation-absorbant materials to minimize reflectivity.
'Double-W' trailing-edge incorporating elevons and drag rudders outboard of engines.
Two side by side weapons bays in lower centrebody each have small, drop-down spoiler panels ahead of doors to generate vortexes, ensuring a clean weapons release.
Engines are fed by S-shaped air ducts, with 3-pointed splitter plates ahead of inlets which remove boundary layer and provide secondary air flow for cooling and IR emissions control.
These 2D nozzles reduce thermal and acoustic signatures.
Two V-shaped overwing exhausts set well forward of trailing-edge.
Titanium on wing surface behind engine outlet, wingtips and leading-edges have dielectric covering of aerofoil section to mask radar-dissipating with a sawtooth construction.
The main APQ-181 radar, similar to the APG-10 in F-15C/D/E, is a synthetic-aperture type and has 21 operational modes, including coherent mapping.
A total of 80,000 hours of testing was done on the B-2's components.
These include 24,000 hours in the wind tunnel, 44,000 hours of avionics testing and 6,000 hours of full-scale 'plastic bird' control system tests.
Flight testing of the B-2 to total 4,000 hours with six aircraft.
The prototype is built on production tooling to an accuracy of +/-6.3 mm from tip to tip.
Developement of the B-2 required nearly 900 new materials and processes to be invented, including over 4,000 subcontractors throughout the USA.
POWER PLANT:
Four 8618 kg (17,300 lb) General Electric F118-GE-100 non-afterburning, dry thrust turbofans mounted in pairs within wing structure.
Total thrust of 34,472 kg (76 000 lb, 169 kN)
In-flight refuelling receptacle in centrebody spine.
ACCOMMODATION:
Two crew members, with upward-firing ejection seats: pilot to port, mission commander/instructor pilot to starboard.
Provision for third member behind commander.
Both forward positions have conventional control columns.
Flight, engine, sensor and systems information presented on nine-tube EFIS display.
ARMAMENT:
Boeing rotary launcher assembly (RLA) in each of two side by side weapons bays in lower centrebody, each detachable for loading at weapons dump with up to eight large stores each.
The total capacity of of the RLA include 16 AGM-129 ACMs.
Alternative weapons include:
16 B61 tactical/strategic or 16 B83 strategic free-fall nuclear bombs
80 Mk 82 500 lb bombs
16 Joint Direct Attack Munitions
16 Mk 84 2,000 lb bombs
36 M117 750 lb fire bombs
36 CBU-87/89/97/98 cluster bombs
80 Mk 36 560 lb or Mk 62 sea mines
Stores of 1,000 lb and below held in four (two per weapons bay) bomb rack assemblies (BRA)
http://www.chinfo.navy.mil/navpalib/%20factfile/aircraft/ea6b.gif
Omega Class Surveilance Craft: EA-6B Prowler
Cost: $250,000.
STRUCTURE:
Wings as for A-6E but reinforced to allow for greater gross weight, fatique life and a 5.5 g load factor.
Fuselage as for A-6E but lengthened by 1.37 m (4 ft 6 in).
POWER PLANT:
Two Pratt & Whitney J52-P-408 turbojets, each rated at 49.8 kN (11,200 lb st).
ADVCAP retrofitted with 53.38 kN (12,000 lb st) J52-P-409 engines.
ACCOMMODATION:
Crew of four under two separate upware-opening canopies.
Martin-Baker GRUEA 7 ejection seats for crew.
Two additional crewmen are ECM Officers to operate the ALQ-99 equipment from the rear cockpit.
Either ECMO can independently detect, assign, adjust and monitor the jammers.
The ECMO in the starboard front seat is responsible for communications, navigation defensive ECM and chaff dispending.
AVIONICS:
AN/ALQ-99F tactical jamming system in five integrally powered pods with a total of 10 jamming transmitters.
Each pod covers one of seven frequency bands.
Sensitive surveillance receivers in the fintop pod for long-range detection of radars.
Emitter information is fed to a central digital computer (AN/AYK-14 in ICAP-2 aircrafts) that processes the signals for display and recording.
Detection, identification, direction-finding and jammer set-on sequence can be performed automatically or with manual assistance from crew.
PRB Associates AN/TSQ-142 tactical mission support system.
Teledyne Systems AN/ASN-123 navigation system with digital display group.
ARMAMENT:
Originally unarmed, but currently capable of carrying Texas Instruments AGM-88A HARM anti-radar missiles underwing.
Four underwing hardpoints on ICAP-2 aircraft, six on ADVCAP EA-6B.
http://www.wpafb.af.mil/museum/%20arm/arm31.jpg
Neutron Bomb
This perticular item is available only after an extensive backgrouond check. There is currently no set price so an offers may be negotiated. Available only in one kilotonne form and is capable of adminstering nuclear material over a 5 mile radius.
http://www.afrotc.tcu.edu/photos/%20aircraft/f117/f117_5.jpg
Delta Class Strike Cruiser: F-17 Nighthawk
Cost: $250,000
DESIGN FEATURES:
Multi-faceted airframe designed to reflect radar energy away from originating transmitter, particularly downward-looking AEW aircraft.
Use of a highly angular type of flying wing basic design (based on relaxed stability and controlled via a quadreplex fly-by-wire control system) with a butterfly tail and elements of lifting-body vehicle design.
The concept is to refelct incoming electromagnetic energy and other radiation in all directions, except the originating emitter.
Vortexes from many sharp edges, including leading-edge of wing, designed to form co-ordinated lifting airflow pattern
wings have 67 degrees 30' sweepback, all doors and access panels have serrated edges to suppress radar reflection
boom refuelling receptacle on port side of top plate, aft of cockpit. Frontal radar cross-section estimated as 0.01 m2 (0.1 sq ft).
The F-117A also has no active radars, unlike conventional warplanes. Instead, it uses a search rada being taken by an advanced passive system based on IR sensors and that of the Doppler navigation system by high-quality INS.
The F-117A also has internal accommodation for small warload of "smart" weapons, thus also reduces the aircrafts radar signature, with the absence of protruding hardpoints.
POWER PLANT:
Two 48.0 kN (10,800 lb st) class General Electric F404-GE-F1D2 dry thrust non-augmented turbofans.
Rectangular overwing air intakes with heated grid for anti-icing and low observability.
Auxiliary air intake doors in horizontal surface immediately to the rear.
Part of cold air ingested bypasses engine and is mixed with exhaust gases for cooling.
Narrow-slot 'platypus' exhausts, designed by Astech/MCI, in rear fuselage, with extended lower lip, surrounded by heat tiles of type used on Space Shuttle and with 11 vertical, internal guide vanes.
In-flight refuelling receptacle in decking aft of cockpit. Optional drop tank on internal weapons pylon.
ARMAMENT:
Full range of USAF tactical fighter ordnance, principally two 2000 lb bombs:
BLU-109B low-level laser-guided or GBU-10/GBU-27 laser-guided glide weapons
Alternatively, AGM-65 Maverick or AGM-88 HARM ASMs.
Provision for AIM-9 Sidewinder (against AWACS aircraft).
Internal carriage on two extendible beams in weapon bay. (Only missiles with seeker heads extended below aircraft prior to launch; bombs released from within weapons bay.)
http://www.capitolsource.net/%20images/prog/b2.jpg
Alpha Class Bomber Plane: B2
Cost: $450,000
DESIGN FEATURES:
The whole aircraft is the design of the relaxed-stability type, a flying wing with straight leading-edges swept at 40° with a W-shaped trailing edges.
Emphasis was placed on smooth surfaces with blended flight deck and nacelle bulges.
Use of radiation-absorbant materials to minimize reflectivity.
'Double-W' trailing-edge incorporating elevons and drag rudders outboard of engines.
Two side by side weapons bays in lower centrebody each have small, drop-down spoiler panels ahead of doors to generate vortexes, ensuring a clean weapons release.
Engines are fed by S-shaped air ducts, with 3-pointed splitter plates ahead of inlets which remove boundary layer and provide secondary air flow for cooling and IR emissions control.
These 2D nozzles reduce thermal and acoustic signatures.
Two V-shaped overwing exhausts set well forward of trailing-edge.
Titanium on wing surface behind engine outlet, wingtips and leading-edges have dielectric covering of aerofoil section to mask radar-dissipating with a sawtooth construction.
The main APQ-181 radar, similar to the APG-10 in F-15C/D/E, is a synthetic-aperture type and has 21 operational modes, including coherent mapping.
A total of 80,000 hours of testing was done on the B-2's components.
These include 24,000 hours in the wind tunnel, 44,000 hours of avionics testing and 6,000 hours of full-scale 'plastic bird' control system tests.
Flight testing of the B-2 to total 4,000 hours with six aircraft.
The prototype is built on production tooling to an accuracy of +/-6.3 mm from tip to tip.
Developement of the B-2 required nearly 900 new materials and processes to be invented, including over 4,000 subcontractors throughout the USA.
POWER PLANT:
Four 8618 kg (17,300 lb) General Electric F118-GE-100 non-afterburning, dry thrust turbofans mounted in pairs within wing structure.
Total thrust of 34,472 kg (76 000 lb, 169 kN)
In-flight refuelling receptacle in centrebody spine.
ACCOMMODATION:
Two crew members, with upward-firing ejection seats: pilot to port, mission commander/instructor pilot to starboard.
Provision for third member behind commander.
Both forward positions have conventional control columns.
Flight, engine, sensor and systems information presented on nine-tube EFIS display.
ARMAMENT:
Boeing rotary launcher assembly (RLA) in each of two side by side weapons bays in lower centrebody, each detachable for loading at weapons dump with up to eight large stores each.
The total capacity of of the RLA include 16 AGM-129 ACMs.
Alternative weapons include:
16 B61 tactical/strategic or 16 B83 strategic free-fall nuclear bombs
80 Mk 82 500 lb bombs
16 Joint Direct Attack Munitions
16 Mk 84 2,000 lb bombs
36 M117 750 lb fire bombs
36 CBU-87/89/97/98 cluster bombs
80 Mk 36 560 lb or Mk 62 sea mines
Stores of 1,000 lb and below held in four (two per weapons bay) bomb rack assemblies (BRA)
http://www.chinfo.navy.mil/navpalib/%20factfile/aircraft/ea6b.gif
Omega Class Surveilance Craft: EA-6B Prowler
Cost: $250,000.
STRUCTURE:
Wings as for A-6E but reinforced to allow for greater gross weight, fatique life and a 5.5 g load factor.
Fuselage as for A-6E but lengthened by 1.37 m (4 ft 6 in).
POWER PLANT:
Two Pratt & Whitney J52-P-408 turbojets, each rated at 49.8 kN (11,200 lb st).
ADVCAP retrofitted with 53.38 kN (12,000 lb st) J52-P-409 engines.
ACCOMMODATION:
Crew of four under two separate upware-opening canopies.
Martin-Baker GRUEA 7 ejection seats for crew.
Two additional crewmen are ECM Officers to operate the ALQ-99 equipment from the rear cockpit.
Either ECMO can independently detect, assign, adjust and monitor the jammers.
The ECMO in the starboard front seat is responsible for communications, navigation defensive ECM and chaff dispending.
AVIONICS:
AN/ALQ-99F tactical jamming system in five integrally powered pods with a total of 10 jamming transmitters.
Each pod covers one of seven frequency bands.
Sensitive surveillance receivers in the fintop pod for long-range detection of radars.
Emitter information is fed to a central digital computer (AN/AYK-14 in ICAP-2 aircrafts) that processes the signals for display and recording.
Detection, identification, direction-finding and jammer set-on sequence can be performed automatically or with manual assistance from crew.
PRB Associates AN/TSQ-142 tactical mission support system.
Teledyne Systems AN/ASN-123 navigation system with digital display group.
ARMAMENT:
Originally unarmed, but currently capable of carrying Texas Instruments AGM-88A HARM anti-radar missiles underwing.
Four underwing hardpoints on ICAP-2 aircraft, six on ADVCAP EA-6B.
http://www.wpafb.af.mil/museum/%20arm/arm31.jpg
Neutron Bomb
This perticular item is available only after an extensive backgrouond check. There is currently no set price so an offers may be negotiated. Available only in one kilotonne form and is capable of adminstering nuclear material over a 5 mile radius.