XF-2 (Imperial Experimental Airframe)

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XF-2 Imperial Experimental Airframe

Description
Mission ProfileExperimental Trans-Atmospheric Fighter Design
Crew1 pilot
First FlightUnknown
Manufacturer(s)Royal Imperial Labs
Operator(s)Royal Imperial Air Force
VariantsNone
Length 15 meters
Wingspan 10 meters
Height 4 meters
Main Systems
PowerplantLiquid Cesium and Jet Fuel
Propulsion1 x Royal Imperial Labs Series-1 Ramjet
1 x Royal Imperial Labs Series-1 Ion Engine
Avionics PackageStandard Fly-By-Wire System
Control SystemsAeroelastic Control Surface for Atmospheric Flight
SensorsNone
CommunicationsRoyal Imperial Labs Series-1 Radio Transceiver
Performance Ratings
Maximum AirspeedMach 1
Cruising Airspeed1300KPH km/h
Acceleration Rate30 km/h/s
Maximum VelocityEscape Velocity km/s
Operation Time 1 Hour hours
Combat Systems
Fixed WeaponsNone
Variable PayloadNone
ArmorReinforced Airframe
ShieldsNone
CountermeasuresNone

The XF-2 program continued using the XF-1 airframe, but served as an ion engine test bed. While highly successful in terms of space use, it could not achieve escape velocity at all, because the ion engine would not function in atmosphere.

After two flights, one launched from space to test the ion engine and one from a runway to test the use of the ion engine in boosting the aircraft to escape velocity, the XF-2 program was terminated and the staff were reassigned to the XF-3 program.

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