The Flickr Usarmycombatcapabilitiesdevelopmentcommand Image Generatr

This image is excerpted from a U.S. GAO report:
www.gao.gov/products/GAO-24-106297

Federal Research: Key Practices for Scientific Program Managers

Note: National Science Foundation, National Center for Science and Engineering Statistics, Survey of Federal Funds for Research and Development: Fiscal Years 2020–21. NSF 22-323 (Alexandria, VA: 2022). NSF referred to these FY 2021 data as 'preliminary' in survey documentation because these data were updated in the subsequent volume of the survey. We refer to the FY 2021 data as 'estimates' throughout this appendix.

Hyperion was designed and refined 3-4 years ago, and a militarized version was created simaltaniously. Plus a larger 145" Length C version for 500 lbs payloads

www.ioaircraft.com/hypersonic/hyperion-b.php

Hyper B, at Mach 15, 500-600 NM range from launch to target. 180 miles per minute. For longer range, Mach 10-12 for 1,000 NM range (fuel conservation) for 200-220 seconds under power.

HAWC, the scramjet missile DOD is funding is Mach 5.6sh and low end copy of the X-51, kero fueled.

www.ioaircraft.com/hypersonic/hyperion-b.php

Total Length: 88"
Wingspan: 19.5"
Payload: 25-45 LBS Ordnance Package
Velocity: Mach 10-15

Fuel: Hydrogen (16,000 PSI) 120 Seconds under power
Range: 500-1,000+ NM
Estimated Price in Production: $250,000-$300,000 ea


Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

Hyperion was designed and refined 3-4 years ago, and a militarized version was created simaltaniously. Plus a larger 145" Length C version for 500 lbs payloads

www.ioaircraft.com/hypersonic/hyperion-b.php

Hyper B, at Mach 15, 500-600 NM range from launch to target. 180 miles per minute. For longer range, Mach 10-12 for 1,000 NM range (fuel conservation) for 200-220 seconds under power.

HAWC, the scramjet missile DOD is funding is Mach 5.6sh and low end copy of the X-51, kero fueled.

www.ioaircraft.com/hypersonic/hyperion-b.php

Total Length: 88"
Wingspan: 19.5"
Payload: 25-45 LBS Ordnance Package
Velocity: Mach 10-15

Fuel: Hydrogen (16,000 PSI) 120 Seconds under power
Range: 500-1,000+ NM
Estimated Price in Production: $250,000-$300,000 ea


Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

Hyperion was designed and refined 3-4 years ago, and a militarized version was created simaltaniously. Plus a larger 145" Length C version for 500 lbs payloads

www.ioaircraft.com/hypersonic/hyperion-b.php

Hyper B, at Mach 15, 500-600 NM range from launch to target. 180 miles per minute. For longer range, Mach 10-12 for 1,000 NM range (fuel conservation) for 200-220 seconds under power.

HAWC, the scramjet missile DOD is funding is Mach 5.6sh and low end copy of the X-51, kero fueled.

www.ioaircraft.com/hypersonic/hyperion-b.php

Total Length: 88"
Wingspan: 19.5"
Payload: 25-45 LBS Ordnance Package
Velocity: Mach 10-15

Fuel: Hydrogen (16,000 PSI) 120 Seconds under power
Range: 500-1,000+ NM
Estimated Price in Production: $250,000-$300,000 ea


Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

Hyperion was designed and refined 3-4 years ago, and a militarized version was created simaltaniously. Plus a larger 145" Length C version for 500 lbs payloads

www.ioaircraft.com/hypersonic/hyperion-b.php

Hyper B, at Mach 15, 500-600 NM range from launch to target. 180 miles per minute. For longer range, Mach 10-12 for 1,000 NM range (fuel conservation) for 200-220 seconds under power.

HAWC, the scramjet missile DOD is funding is Mach 5.6sh and low end copy of the X-51, kero fueled.

www.ioaircraft.com/hypersonic/hyperion-b.php

Total Length: 88"
Wingspan: 19.5"
Payload: 25-45 LBS Ordnance Package
Velocity: Mach 10-15

Fuel: Hydrogen (16,000 PSI) 120 Seconds under power
Range: 500-1,000+ NM
Estimated Price in Production: $250,000-$300,000 ea


Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

Hyperion was designed and refined 3-4 years ago, and a militarized version was created simaltaniously. Plus a larger 145" Length C version for 500 lbs payloads

www.ioaircraft.com/hypersonic/hyperion-b.php

Hyper B, at Mach 15, 500-600 NM range from launch to target. 180 miles per minute. For longer range, Mach 10-12 for 1,000 NM range (fuel conservation) for 200-220 seconds under power.

HAWC, the scramjet missile DOD is funding is Mach 5.6sh and low end copy of the X-51, kero fueled.

www.ioaircraft.com/hypersonic/hyperion-b.php

Total Length: 88"
Wingspan: 19.5"
Payload: 25-45 LBS Ordnance Package
Velocity: Mach 10-15

Fuel: Hydrogen (16,000 PSI) 120 Seconds under power
Range: 500-1,000+ NM
Estimated Price in Production: $250,000-$300,000 ea


Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

Hyperion was designed and refined 3-4 years ago, and a militarized version was created simaltaniously. Plus a larger 145" Length C version for 500 lbs payloads

www.ioaircraft.com/hypersonic/hyperion-b.php

Hyper B, at Mach 15, 500-600 NM range from launch to target. 180 miles per minute. For longer range, Mach 10-12 for 1,000 NM range (fuel conservation) for 200-220 seconds under power.

HAWC, the scramjet missile DOD is funding is Mach 5.6sh and low end copy of the X-51, kero fueled.

www.ioaircraft.com/hypersonic/hyperion-b.php

Total Length: 88"
Wingspan: 19.5"
Payload: 25-45 LBS Ordnance Package
Velocity: Mach 10-15

Fuel: Hydrogen (16,000 PSI) 120 Seconds under power
Range: 500-1,000+ NM
Estimated Price in Production: $250,000-$300,000 ea


Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

VSFR-2 Self Propelled Hypersonic Cruise Missile (IT1). Update from early version in 2017

www.ioaircraft.com/hypersonic/vsfr2.php

Total Length: 120"

Wingspan: 24"

Payload: 20-50 LBS Ordnance Package

Velocity: Mach 8-10

Propulsion: U-TBCC

Fuel: Hydrogen (16,000 PSI) / Kero / Apx 7 Gallons

Range: 1,000+ NM

Estimated Price in Production: $250,000 ea

Hydrogen: (16,000 PSI) / Kero / Apx 7 Gallons

NASA
Jet Propulsion Laboratory
AFOSR
Office of Naval Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Airbus
Airbus Defence
BAE Systems
U.S. Army Combat Capabilities Development Command
The U.S. Army Research Laboratory
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls Royce
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
ICAO
Dassault Aviation
United States Space Force
Northrop Grumman Corporation
Hermeus
Aerojet Rocketdyne
Boom Supersonic
Defence Australia

Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

VSFR-2 Self Propelled Hypersonic Cruise Missile (IT1). Update from early version in 2017

www.ioaircraft.com/hypersonic/vsfr2.php

Total Length: 120"

Wingspan: 24"

Payload: 20-50 LBS Ordnance Package

Velocity: Mach 8-10

Propulsion: U-TBCC

Fuel: Hydrogen (16,000 PSI) / Kero / Apx 7 Gallons

Range: 1,000+ NM

Estimated Price in Production: $250,000 ea

Hydrogen: (16,000 PSI) / Kero / Apx 7 Gallons

NASA
Jet Propulsion Laboratory
AFOSR
Office of Naval Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Airbus
Airbus Defence
BAE Systems
U.S. Army Combat Capabilities Development Command
The U.S. Army Research Laboratory
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls Royce
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
ICAO
Dassault Aviation
United States Space Force
Northrop Grumman Corporation
Hermeus
Aerojet Rocketdyne
Boom Supersonic
Defence Australia

Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

VSFR-2 Self Propelled Hypersonic Cruise Missile (IT1). Update from early version in 2017

www.ioaircraft.com/hypersonic/vsfr2.php

Total Length: 120"

Wingspan: 24"

Payload: 20-50 LBS Ordnance Package

Velocity: Mach 8-10

Propulsion: U-TBCC

Fuel: Hydrogen (16,000 PSI) / Kero / Apx 7 Gallons

Range: 1,000+ NM

Estimated Price in Production: $250,000 ea

Hydrogen: (16,000 PSI) / Kero / Apx 7 Gallons

NASA
Jet Propulsion Laboratory
AFOSR
Office of Naval Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Airbus
Airbus Defence
BAE Systems
U.S. Army Combat Capabilities Development Command
The U.S. Army Research Laboratory
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls Royce
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
ICAO
Dassault Aviation
United States Space Force
Northrop Grumman Corporation
Hermeus
Aerojet Rocketdyne
Boom Supersonic
Defence Australia

Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

VSFR-2 Self Propelled Hypersonic Cruise Missile (IT1). Update from early version in 2017

www.ioaircraft.com/hypersonic/vsfr2.php

Total Length: 120"

Wingspan: 24"

Payload: 20-50 LBS Ordnance Package

Velocity: Mach 8-10

Propulsion: U-TBCC

Fuel: Hydrogen (16,000 PSI) / Kero / Apx 7 Gallons

Range: 1,000+ NM

Estimated Price in Production: $250,000 ea

Hydrogen: (16,000 PSI) / Kero / Apx 7 Gallons

NASA
Jet Propulsion Laboratory
AFOSR
Office of Naval Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Airbus
Airbus Defence
BAE Systems
U.S. Army Combat Capabilities Development Command
The U.S. Army Research Laboratory
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls Royce
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
ICAO
Dassault Aviation
United States Space Force
Northrop Grumman Corporation
Hermeus
Aerojet Rocketdyne
Boom Supersonic
Defence Australia

Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

VSFR-2 Self Propelled Hypersonic Cruise Missile (IT1). Update from early version in 2017

www.ioaircraft.com/hypersonic/vsfr2.php

Total Length: 120"

Wingspan: 24"

Payload: 20-50 LBS Ordnance Package

Velocity: Mach 8-10

Propulsion: U-TBCC

Fuel: Hydrogen (16,000 PSI) / Kero / Apx 7 Gallons

Range: 1,000+ NM

Estimated Price in Production: $250,000 ea

Hydrogen: (16,000 PSI) / Kero / Apx 7 Gallons

NASA
Jet Propulsion Laboratory
AFOSR
Office of Naval Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Airbus
Airbus Defence
BAE Systems
U.S. Army Combat Capabilities Development Command
The U.S. Army Research Laboratory
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls Royce
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
ICAO
Dassault Aviation
United States Space Force
Northrop Grumman Corporation
Hermeus
Aerojet Rocketdyne
Boom Supersonic
Defence Australia

Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

VSFR-2 Self Propelled Hypersonic Cruise Missile (IT1). Update from early version in 2017

www.ioaircraft.com/hypersonic/vsfr2.php

Total Length: 120"

Wingspan: 24"

Payload: 20-50 LBS Ordnance Package

Velocity: Mach 8-10

Propulsion: U-TBCC

Fuel: Hydrogen (16,000 PSI) / Kero / Apx 7 Gallons

Range: 1,000+ NM

Estimated Price in Production: $250,000 ea

Hydrogen: (16,000 PSI) / Kero / Apx 7 Gallons

NASA
Jet Propulsion Laboratory
AFOSR
Office of Naval Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Airbus
Airbus Defence
BAE Systems
U.S. Army Combat Capabilities Development Command
The U.S. Army Research Laboratory
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls Royce
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
ICAO
Dassault Aviation
United States Space Force
Northrop Grumman Corporation
Hermeus
Aerojet Rocketdyne
Boom Supersonic
Defence Australia

Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

VSFR-2 Self Propelled Hypersonic Cruise Missile (IT1). Update from early version in 2017

www.ioaircraft.com/hypersonic/vsfr2.php

Total Length: 120"

Wingspan: 24"

Payload: 20-50 LBS Ordnance Package

Velocity: Mach 8-10

Propulsion: U-TBCC

Fuel: Hydrogen (16,000 PSI) / Kero / Apx 7 Gallons

Range: 1,000+ NM

Estimated Price in Production: $250,000 ea

Hydrogen: (16,000 PSI) / Kero / Apx 7 Gallons

NASA
Jet Propulsion Laboratory
AFOSR
Office of Naval Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Airbus
Airbus Defence
BAE Systems
U.S. Army Combat Capabilities Development Command
The U.S. Army Research Laboratory
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls Royce
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
ICAO
Dassault Aviation
United States Space Force
Northrop Grumman Corporation
Hermeus
Aerojet Rocketdyne
Boom Supersonic
Defence Australia

Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

VSFR-2 Self Propelled Hypersonic Cruise Missile (IT1). Update from early version in 2017

www.ioaircraft.com/hypersonic/vsfr2.php

Total Length: 120"

Wingspan: 24"

Payload: 20-50 LBS Ordnance Package

Velocity: Mach 8-10

Propulsion: U-TBCC

Fuel: Hydrogen (16,000 PSI) / Kero / Apx 7 Gallons

Range: 1,000+ NM

Estimated Price in Production: $250,000 ea

Hydrogen: (16,000 PSI) / Kero / Apx 7 Gallons

NASA
Jet Propulsion Laboratory
AFOSR
Office of Naval Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Airbus
Airbus Defence
BAE Systems
U.S. Army Combat Capabilities Development Command
The U.S. Army Research Laboratory
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls Royce
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
ICAO
Dassault Aviation
United States Space Force
Northrop Grumman Corporation
Hermeus
Aerojet Rocketdyne
Boom Supersonic
Defence Australia

Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

VSFR-2 Self Propelled Hypersonic Cruise Missile (IT1). Update from early version in 2017

www.ioaircraft.com/hypersonic/vsfr2.php

Total Length: 120"

Wingspan: 24"

Payload: 20-50 LBS Ordnance Package

Velocity: Mach 8-10

Propulsion: U-TBCC

Fuel: Hydrogen (16,000 PSI) / Kero / Apx 7 Gallons

Range: 1,000+ NM

Estimated Price in Production: $250,000 ea

Hydrogen: (16,000 PSI) / Kero / Apx 7 Gallons

NASA
Jet Propulsion Laboratory
AFOSR
Office of Naval Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Airbus
Airbus Defence
BAE Systems
U.S. Army Combat Capabilities Development Command
The U.S. Army Research Laboratory
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls Royce
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
ICAO
Dassault Aviation
United States Space Force
Northrop Grumman Corporation
Hermeus
Aerojet Rocketdyne
Boom Supersonic
Defence Australia

Hypersonic Cruise Missile, Gambit. RDE, rotating detonating engine, hypersonic fighter, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

XH - Talon - 8th Gen VTOL Hypersonic UCAV (Iteration 1 Finalized)

Sanitized, but iteration 1 is complete, will be more details on our website within a week or two. Brand new design, not graphics. Months of hashing out physics, configuration, cfd, etc.

XH Talon: 8th Gen VTOL Mach 9-14 Hypersonic Super Maneuvering UCAV

49' Length, 25' Span, Wings Folded: 16' Span

www.ioaircraft.com/technology-hypersonics.php

Link to Engines/Propulsion www.ioaircraft.com/hypersonic/utbcc.php

Link to Hydrogen Conforming Tanks ioaircraft.com/innovation/conformingtanks.php

Link to Graphene www.ioaircraft.com/technology-graphene.php

Link to Super Conducting Motors www.ioaircraft.com/technology-motors.php

Extreme capabilities, unseen by the humans including black programs. H2 fueled (kero based scramjet engines are not able to operate long above M6) with a kero reserve for ferry flights, subsonic, etc. It can adapt in flight from 100% kero through 100% H2 making it an advanced hybrid.

Summary technologies of the below (real, not academics) 49' length, less then 6' height, 25' span

-6000+F thermal resistance (3rd gen, normalizing high hypersonic flight and orbital re-entry making ablatives and ceramics obsolete entirely)

-graphene airframe (33X tensile strength of titanium but 1/100th the weight of styrofoam)

-VTOL (advanced vtol capabilities, which every aspect is composites)

-u-tbcc propulsion (thru m15 in atmosphere, unified turbine based combined cycle dual mode ramjet/scramjet)

-graphene based super conducting motors for the lift fans (no antiquated shaft driven lift fans)

-H2 Compressed, 1,600 gallons 16,000 PSI (already flown, and patented, publicly, 2nd gen is 16,000 PSI)

-400 gallon kero reserve (hybrid capable)

-Internal bay 154" length to accommodate 1 2,000 JDAM or 3 500 LBS and anything else in between

-3,000+NM RANGE from subsonic through hypersonic, ie Mach 9-14. Super Cruise is an estimated Mach 3. Is able to operate in ramjet mode as well, not just scramjet mode.

-The payload bay can also house a range extender tank conforming internally adding an additional 1,000+ nm range under power for longer range flights used for ferrying and also during intelligence gathering operations, mainly over russia and china.

-Folding wings (16' span folded) for naval operations + Internal tail hook

-Overall weight, at max payload of 3,000 LBS, Kero, and H2, apx 12,300 LBS (Less then the empty weight of an F-35. This is because H2 but also graphene airframe, and graphene/carbide hybrid surfacing)

-USAF version, just remove the lift fans and add more fuel capacity, give an additional 1,000+nm range internally

VTOL, ngad, ucav, arrw, hawc, glidebreaker, hypersonic, hypersonics, ksc, capecanaveral, spacecoast, spaceforce, hydrogen, graphene, darpa, airforceresearchlab, afwerx, defwerx, nasa, aviation, airbus, engineering, defense, icao, aiaa, nro, nrl, navsea, onr, afwerx, hsvtol, tbcc, darkstar, aerothermaldynamics, fighterjet, hypersonicfighter, innovation, aerospace, airplane

Virgin Orbit
Virgin Galactic
Sierra Nevada Corporation
Aevum Inc
NASA
NASA Jet Propulsion Laboratory
AFOSR, Air Force Office of Scientific Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Firefly Aerospace
ESA - European Space Agency
SpaceX
Axiom Space
Airbus
Airbus Defence
BAE Systems
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls-Royce plc
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
BlackSky
United Launch Alliance
TÉLÉSAT
ONE.Web
ICAO - International Civil Aviation Organization
Dassault Aviation
United States Space Force
Blue Origin
Northrop Grumman Corporation
Arianespace

hypersonic fighter, Hpersonic UCAV, Hypersonic UAV, VTOL Hypersonics, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

XH - Talon - 8th Gen VTOL Hypersonic UCAV (Iteration 1 Finalized)

Sanitized, but iteration 1 is complete, will be more details on our website within a week or two. Brand new design, not graphics. Months of hashing out physics, configuration, cfd, etc.

XH Talon: 8th Gen VTOL Mach 9-14 Hypersonic Super Maneuvering UCAV

49' Length, 25' Span, Wings Folded: 16' Span

www.ioaircraft.com/technology-hypersonics.php

Link to Engines/Propulsion www.ioaircraft.com/hypersonic/utbcc.php

Link to Hydrogen Conforming Tanks ioaircraft.com/innovation/conformingtanks.php

Link to Graphene www.ioaircraft.com/technology-graphene.php

Link to Super Conducting Motors www.ioaircraft.com/technology-motors.php

Extreme capabilities, unseen by the humans including black programs. H2 fueled (kero based scramjet engines are not able to operate long above M6) with a kero reserve for ferry flights, subsonic, etc. It can adapt in flight from 100% kero through 100% H2 making it an advanced hybrid.

Summary technologies of the below (real, not academics) 49' length, less then 6' height, 25' span

-6000+F thermal resistance (3rd gen, normalizing high hypersonic flight and orbital re-entry making ablatives and ceramics obsolete entirely)

-graphene airframe (33X tensile strength of titanium but 1/100th the weight of styrofoam)

-VTOL (advanced vtol capabilities, which every aspect is composites)

-u-tbcc propulsion (thru m15 in atmosphere, unified turbine based combined cycle dual mode ramjet/scramjet)

-graphene based super conducting motors for the lift fans (no antiquated shaft driven lift fans)

-H2 Compressed, 1,600 gallons 16,000 PSI (already flown, and patented, publicly, 2nd gen is 16,000 PSI)

-400 gallon kero reserve (hybrid capable)

-Internal bay 154" length to accommodate 1 2,000 JDAM or 3 500 LBS and anything else in between

-3,000+NM RANGE from subsonic through hypersonic, ie Mach 9-14. Super Cruise is an estimated Mach 3. Is able to operate in ramjet mode as well, not just scramjet mode.

-The payload bay can also house a range extender tank conforming internally adding an additional 1,000+ nm range under power for longer range flights used for ferrying and also during intelligence gathering operations, mainly over russia and china.

-Folding wings (16' span folded) for naval operations + Internal tail hook

-Overall weight, at max payload of 3,000 LBS, Kero, and H2, apx 12,300 LBS (Less then the empty weight of an F-35. This is because H2 but also graphene airframe, and graphene/carbide hybrid surfacing)

-USAF version, just remove the lift fans and add more fuel capacity, give an additional 1,000+nm range internally

VTOL, ngad, ucav, arrw, hawc, glidebreaker, hypersonic, hypersonics, ksc, capecanaveral, spacecoast, spaceforce, hydrogen, graphene, darpa, airforceresearchlab, afwerx, defwerx, nasa, aviation, airbus, engineering, defense, icao, aiaa, nro, nrl, navsea, onr, afwerx, hsvtol, tbcc, darkstar, aerothermaldynamics, fighterjet, hypersonicfighter, innovation, aerospace, airplane

Virgin Orbit
Virgin Galactic
Sierra Nevada Corporation
Aevum Inc
NASA
NASA Jet Propulsion Laboratory
AFOSR, Air Force Office of Scientific Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Firefly Aerospace
ESA - European Space Agency
SpaceX
Axiom Space
Airbus
Airbus Defence
BAE Systems
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls-Royce plc
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
BlackSky
United Launch Alliance
TÉLÉSAT
ONE.Web
ICAO - International Civil Aviation Organization
Dassault Aviation
United States Space Force
Blue Origin
Northrop Grumman Corporation
Arianespace

hypersonic fighter, Hpersonic UCAV, Hypersonic UAV, VTOL Hypersonics, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

XH - Talon - 8th Gen VTOL Hypersonic UCAV (Iteration 1 Finalized)

Sanitized, but iteration 1 is complete, will be more details on our website within a week or two. Brand new design, not graphics. Months of hashing out physics, configuration, cfd, etc.

XH Talon: 8th Gen VTOL Mach 9-14 Hypersonic Super Maneuvering UCAV

49' Length, 25' Span, Wings Folded: 16' Span

www.ioaircraft.com/technology-hypersonics.php

Link to Engines/Propulsion www.ioaircraft.com/hypersonic/utbcc.php

Link to Hydrogen Conforming Tanks ioaircraft.com/innovation/conformingtanks.php

Link to Graphene www.ioaircraft.com/technology-graphene.php

Link to Super Conducting Motors www.ioaircraft.com/technology-motors.php

Extreme capabilities, unseen by the humans including black programs. H2 fueled (kero based scramjet engines are not able to operate long above M6) with a kero reserve for ferry flights, subsonic, etc. It can adapt in flight from 100% kero through 100% H2 making it an advanced hybrid.

Summary technologies of the below (real, not academics) 49' length, less then 6' height, 25' span

-6000+F thermal resistance (3rd gen, normalizing high hypersonic flight and orbital re-entry making ablatives and ceramics obsolete entirely)

-graphene airframe (33X tensile strength of titanium but 1/100th the weight of styrofoam)

-VTOL (advanced vtol capabilities, which every aspect is composites)

-u-tbcc propulsion (thru m15 in atmosphere, unified turbine based combined cycle dual mode ramjet/scramjet)

-graphene based super conducting motors for the lift fans (no antiquated shaft driven lift fans)

-H2 Compressed, 1,600 gallons 16,000 PSI (already flown, and patented, publicly, 2nd gen is 16,000 PSI)

-400 gallon kero reserve (hybrid capable)

-Internal bay 154" length to accommodate 1 2,000 JDAM or 3 500 LBS and anything else in between

-3,000+NM RANGE from subsonic through hypersonic, ie Mach 9-14. Super Cruise is an estimated Mach 3. Is able to operate in ramjet mode as well, not just scramjet mode.

-The payload bay can also house a range extender tank conforming internally adding an additional 1,000+ nm range under power for longer range flights used for ferrying and also during intelligence gathering operations, mainly over russia and china.

-Folding wings (16' span folded) for naval operations + Internal tail hook

-Overall weight, at max payload of 3,000 LBS, Kero, and H2, apx 12,300 LBS (Less then the empty weight of an F-35. This is because H2 but also graphene airframe, and graphene/carbide hybrid surfacing)

-USAF version, just remove the lift fans and add more fuel capacity, give an additional 1,000+nm range internally

VTOL, ngad, ucav, arrw, hawc, glidebreaker, hypersonic, hypersonics, ksc, capecanaveral, spacecoast, spaceforce, hydrogen, graphene, darpa, airforceresearchlab, afwerx, defwerx, nasa, aviation, airbus, engineering, defense, icao, aiaa, nro, nrl, navsea, onr, afwerx, hsvtol, tbcc, darkstar, aerothermaldynamics, fighterjet, hypersonicfighter, innovation, aerospace, airplane

Virgin Orbit
Virgin Galactic
Sierra Nevada Corporation
Aevum Inc
NASA
NASA Jet Propulsion Laboratory
AFOSR, Air Force Office of Scientific Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Firefly Aerospace
ESA - European Space Agency
SpaceX
Axiom Space
Airbus
Airbus Defence
BAE Systems
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls-Royce plc
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
BlackSky
United Launch Alliance
TÉLÉSAT
ONE.Web
ICAO - International Civil Aviation Organization
Dassault Aviation
United States Space Force
Blue Origin
Northrop Grumman Corporation
Arianespace

hypersonic fighter, Hpersonic UCAV, Hypersonic UAV, VTOL Hypersonics, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia

XH - Talon - 8th Gen VTOL Hypersonic UCAV (Iteration 1 Finalized)

Sanitized, but iteration 1 is complete, will be more details on our website within a week or two. Brand new design, not graphics. Months of hashing out physics, configuration, cfd, etc.

XH Talon: 8th Gen VTOL Mach 9-14 Hypersonic Super Maneuvering UCAV

49' Length, 25' Span, Wings Folded: 16' Span

www.ioaircraft.com/technology-hypersonics.php

Link to Engines/Propulsion www.ioaircraft.com/hypersonic/utbcc.php

Link to Hydrogen Conforming Tanks ioaircraft.com/innovation/conformingtanks.php

Link to Graphene www.ioaircraft.com/technology-graphene.php

Link to Super Conducting Motors www.ioaircraft.com/technology-motors.php

Extreme capabilities, unseen by the humans including black programs. H2 fueled (kero based scramjet engines are not able to operate long above M6) with a kero reserve for ferry flights, subsonic, etc. It can adapt in flight from 100% kero through 100% H2 making it an advanced hybrid.

Summary technologies of the below (real, not academics) 49' length, less then 6' height, 25' span

-6000+F thermal resistance (3rd gen, normalizing high hypersonic flight and orbital re-entry making ablatives and ceramics obsolete entirely)

-graphene airframe (33X tensile strength of titanium but 1/100th the weight of styrofoam)

-VTOL (advanced vtol capabilities, which every aspect is composites)

-u-tbcc propulsion (thru m15 in atmosphere, unified turbine based combined cycle dual mode ramjet/scramjet)

-graphene based super conducting motors for the lift fans (no antiquated shaft driven lift fans)

-H2 Compressed, 1,600 gallons 16,000 PSI (already flown, and patented, publicly, 2nd gen is 16,000 PSI)

-400 gallon kero reserve (hybrid capable)

-Internal bay 154" length to accommodate 1 2,000 JDAM or 3 500 LBS and anything else in between

-3,000+NM RANGE from subsonic through hypersonic, ie Mach 9-14. Super Cruise is an estimated Mach 3. Is able to operate in ramjet mode as well, not just scramjet mode.

-The payload bay can also house a range extender tank conforming internally adding an additional 1,000+ nm range under power for longer range flights used for ferrying and also during intelligence gathering operations, mainly over russia and china.

-Folding wings (16' span folded) for naval operations + Internal tail hook

-Overall weight, at max payload of 3,000 LBS, Kero, and H2, apx 12,300 LBS (Less then the empty weight of an F-35. This is because H2 but also graphene airframe, and graphene/carbide hybrid surfacing)

-USAF version, just remove the lift fans and add more fuel capacity, give an additional 1,000+nm range internally

VTOL, ngad, ucav, arrw, hawc, glidebreaker, hypersonic, hypersonics, ksc, capecanaveral, spacecoast, spaceforce, hydrogen, graphene, darpa, airforceresearchlab, afwerx, defwerx, nasa, aviation, airbus, engineering, defense, icao, aiaa, nro, nrl, navsea, onr, afwerx, hsvtol, tbcc, darkstar, aerothermaldynamics, fighterjet, hypersonicfighter, innovation, aerospace, airplane

Virgin Orbit
Virgin Galactic
Sierra Nevada Corporation
Aevum Inc
NASA
NASA Jet Propulsion Laboratory
AFOSR, Air Force Office of Scientific Research
Defense Advanced Research Projects Agency
AFWERX
United States Air Force
Air Force Research Laboratory
Firefly Aerospace
ESA - European Space Agency
SpaceX
Axiom Space
Airbus
Airbus Defence
BAE Systems
Northrop Grumman Corporation
Lockheed Martin
Raytheon Technologies
Rolls-Royce plc
National Reconnaissance Office
The Aerospace Corporation
Collins Aerospace
BlackSky
United Launch Alliance
TÉLÉSAT
ONE.Web
ICAO - International Civil Aviation Organization
Dassault Aviation
United States Space Force
Blue Origin
Northrop Grumman Corporation
Arianespace

hypersonic fighter, Hpersonic UCAV, Hypersonic UAV, VTOL Hypersonics, ngad, ucav, navsea, arrw, hawc, hypersonic, hypersonics, ksc, cape canaveral, space coast, space force, hydrogen, darpa, defwerx, aviation, engineering, defense, aiaa, nro, nrl, navsea, onr, afrl, hsvtol , tbcc, darkstar, aero thermal dynamics, innovation, aerospace, airplane, osd, Scramjet, graphene, NASA, National Aeronautics and Space Administration, Jet Propulsion Laboratory, AFOSR, Air Force Office of Scientific Research, Office of Naval Research, Defense Advanced Research Projects Agency, DARPA, AFWERX, United States Air Force, Air Force Research Laboratory, Airbus, Airbus Defence, BAE Systems, US Army Combat Capabilities Development Command, US Army Research Laboratory, Northrop Grumman Corporation, Lockheed Martin, Raytheon Technologies, Rolls Royce, National Reconnaissance Office, The Aerospace Corporation, Collins Aerospace, International Civil Aviation Organization, Dassault Aviation, United States Space Force, Northrop Grumman Corporation, Hermeus, Aerojet Rocketdyne, Boom Supersonic, Defence Australia