IO Aircraft
Discovery SSTO V8.2 - Single Stage to Orbit Heavy Lift, Hypersonic Aircraft - 70 TON Payload - IO Aircraft
Discovery SSTO V8.2 - Single Stage to Orbit Heavy Lift, Hypersonic Aircraft - 70 TON Payload - IO Aircraft
IO Aircraft: www.ioaircraft.com/hypersonic/discovery-218.php
Discovery SSTO V8.2 Specs
Length: 218FT/ Span: 102.58FT / Palyload Bay: 60' L X 16' 7" W X 16' 7" H / Span: 70 Ton (140,000 LBS)
Engines: U-TBCC (Unified Turbined Based Combined Cycle) Inc/Zero Atmosphere
Inlets: Adaptive REST, Originally Hapb/Larc NASA
Fuel: 140,000 Gallons 12,000+ PSI H2 / 90,000 Gallons 12,000+ PSI O2
Fuel Weight: Apx 72,000 LBS Total / *If liquid, would be 1.4 Million LBS
Weight: Apx 250,000 LBS EOW/Dry Weight / Apx 510,000 T/O Weight, Max Payload
Airframe: 75+% Proprietary Advanced Composites, 400,000 PSI Tensile Strength Airframe / *NO Ceramic Tiles
Thermals: 6,000F Thermal Resistance
Estimated Cost: $1.2 Billion Each (Fly Away Price) or $900 million in batches of 5
Estimated Launch Cost: Apx $30 Million at 140,000 LBS, Including Maintenance Costs / Under $250 per pound at Maximum Paylaod Wieght *Could Drop to Below $50 per LBS
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Unified Turbine Based Combined Cycle. Current technologies and what Lockheed is trying to force on the Dept of Defense, for that low speed Mach 5 plane DOD gave them $1 billion to build and would disintegrate above Mach 5, is TBCC. 2 separate propulsion systems in the same airframe, which requires TWICE the airframe space to use.
Unified Turbine Based Combined Cycle is 1 propulsion system cutting that airframe deficit in half, and also able to operate above Mach 10 up to Mach 15 in atmosphere, and a simple nozzle modification allows for outside atmosphere rocket mode, ie orbital capable.
Additionally, Reaction Engines maximum air breather mode is Mach 4.5, above that it will explode in flight from internal pressures are too high to operate. Thus, must switch to non air breather rocket mode to operate in atmosphere in hypersonic velocities. Which as a result, makes it not feasible for anything practical. It also takes an immense amount of fuel to function.
Discovery SSTO V8.2 - Single Stage to Orbit Heavy Lift, Hypersonic Aircraft - 70 TON Payload - IO Aircraft
Discovery SSTO V8.2 - Single Stage to Orbit Heavy Lift, Hypersonic Aircraft - 70 TON Payload - IO Aircraft
IO Aircraft: www.ioaircraft.com/hypersonic/discovery-218.php
Discovery SSTO V8.2 Specs
Length: 218FT/ Span: 102.58FT / Palyload Bay: 60' L X 16' 7" W X 16' 7" H / Span: 70 Ton (140,000 LBS)
Engines: U-TBCC (Unified Turbined Based Combined Cycle) Inc/Zero Atmosphere
Inlets: Adaptive REST, Originally Hapb/Larc NASA
Fuel: 140,000 Gallons 12,000+ PSI H2 / 90,000 Gallons 12,000+ PSI O2
Fuel Weight: Apx 72,000 LBS Total / *If liquid, would be 1.4 Million LBS
Weight: Apx 250,000 LBS EOW/Dry Weight / Apx 510,000 T/O Weight, Max Payload
Airframe: 75+% Proprietary Advanced Composites, 400,000 PSI Tensile Strength Airframe / *NO Ceramic Tiles
Thermals: 6,000F Thermal Resistance
Estimated Cost: $1.2 Billion Each (Fly Away Price) or $900 million in batches of 5
Estimated Launch Cost: Apx $30 Million at 140,000 LBS, Including Maintenance Costs / Under $250 per pound at Maximum Paylaod Wieght *Could Drop to Below $50 per LBS
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single stage to orbit, ssto, space plane, falcon heavy, delta iv, hypersonic commercial aircraft, hypersonic commercial plane, hypersonic aircraft, hypersonic plane, ICAO, International Civil Aviation Orginization, hypersonic airline, tbcc, glide breaker, fighter plane, hyperonic fighter, boeing phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, office of naval research, defense advanced research project agency, defense science, missile defense agency, aerospike, hydrogen fueled, hydrogen aircraft, virgin airlines, united airlines, sas, finnair ,emirates airlines, ANA, JAL, airlines, military, physics, airline, british airways, air france, aerion supersonic, aerion, spike aerospace, boom supersonic,
-----------------------------
Unified Turbine Based Combined Cycle. Current technologies and what Lockheed is trying to force on the Dept of Defense, for that low speed Mach 5 plane DOD gave them $1 billion to build and would disintegrate above Mach 5, is TBCC. 2 separate propulsion systems in the same airframe, which requires TWICE the airframe space to use.
Unified Turbine Based Combined Cycle is 1 propulsion system cutting that airframe deficit in half, and also able to operate above Mach 10 up to Mach 15 in atmosphere, and a simple nozzle modification allows for outside atmosphere rocket mode, ie orbital capable.
Additionally, Reaction Engines maximum air breather mode is Mach 4.5, above that it will explode in flight from internal pressures are too high to operate. Thus, must switch to non air breather rocket mode to operate in atmosphere in hypersonic velocities. Which as a result, makes it not feasible for anything practical. It also takes an immense amount of fuel to function.