Difference between revisions of "EB-15"
| Line 1: | Line 1: | ||
==Overview== | ==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 | ||
===Specifications=== | ===Specifications=== | ||
| Line 21: | Line 26: | ||
===Performance=== | ===Performance=== | ||
| − | '''Maximum Speed:''' | + | '''Maximum Speed:''' 1420mph |
| − | '''Combat Radius:''' | + | '''Combat Radius:''' 4,480 mi (3,890 nm, 7,210 km) |
| − | '''Ferry Range:''' | + | '''Ferry Range:''' 11,000 mi (9,560 nm, 15,000 km) |
| − | '''Service Ceiling:''' | + | '''Service Ceiling:''' 92,300ft |
===Armament=== | ===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== | ==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== | ==Usage== | ||
| + | |||
| + | Soon to be demonstrated. | ||
Revision as of 19:40, 3 September 2007
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
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.
