EB-15

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Revision as of 19:48, 3 September 2007 by Artitsa (Talk | contribs)

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Overview

supercritical airfoil for shorter takeoff/landing and fuel efficiency; airframe out of superplastic forming zinc-aluminum; areas under high thermal/mechanical stress needs titanium I think it's called Ti-62222 or something for what they use in the F-22 vertical stabilizers probably out of al-li? Carbon fiber reinforced thermoplastic? we can probably dissolve schiff-base-salt RAM into an epoxyide applique

Corporations / Countries Involved

Artitsa:

  • Nolan-Petyav Aerospace Propulsion Industries
  • Plantir Research Electronic Dynamics Inc.
  • Hyland-Nikolaas Industries

Specifications

Crew: 5; Pilot, Co-Pilot, Navigator, Radar Navigator, Electronics Warfare Operator

Length: 104.7 Meters

Wingspan: 113.2 Meters

Height: 22.8 Meters

Empty Weight: 207,867kg

Payload: 34,815kg

Fuel Capacity: 69,289kg

Powerplant: Six Nolan-Petyav EBE-M390/09-X 79,333 lbf (354 kN) each

Performance

Maximum Speed: 1420mph

Combat Radius: 4,480 mi (3,890 nm, 7,210 km)

Ferry Range: 11,000 mi (9,560 nm, 15,000 km)

Service Ceiling: 92,300ft

Armament

Four Khan type missiles (In Artitsa's case, GSM.38 Jupiter ASM) in internal bay. These can be swapped out for 35,000kg of munitions, including housing for upto 48 AM-98 sized cruisemissiles.

Electronics

  • Athena System
  • Radomes are constructed out of selective bandpass material
  • rearward facing radar
  • missile alert warners
  • super-heterodyne RWR (so you can figure out the bearing of a transmitter)
  • directional RF jammer mounted in the tailfins
  • pod-mounted IR/UV laser jammer
  • INS/GPS navigation
  • self-repairing flight controls
  • multifunction radar, FLIR/EO imager too
  • utilities management for stuff like hydraulics and oxygen and electrical generation
  • stores management for fuel + payload

Usage

Soon to be demonstrated.