IO Aircraft
HVL130 VTOL Hypdersonic Transport Iteration 1 (vertical take off and landing)
HVL130 Condor, VTOL Hypersonic Transport, global point to point capable. www.ioaircraft.com/hypersonic/condor.php
130' length, 22-25 TON cargo bay capacity, H2 fueled, with onboard oxidizer as needed for Mach 15 velocity at 70 mile altitude (above the karman line). Website link: www.ioaircraft.com/hypersonic/condor.php
At apx 100,000-120,000ft, cruise velocity is Mach 8-10, with a 10,000nm range. Cargo bay and cockpit are hemetically sealed, with onboard oxygen supply and environmentals.
The entire cargo bay opens instead of a cargo bay door, while the nose gear retracts on the ground providing 8 1/2 ft of clearance into the bay.
*This same engineering principle that applies to Condor, can be scaled up further, with a 50-100 ton cargo capacity.
Propulsion for this aircraft is extensive:
2 U-TBCC (Unified Turbine Based Combine Cycle / Dual Mode Scramjet (300,000 LBS Thrust)
5 H2/O2 Compressed Fueled Bell Nozzle Rockets. No turbo pumps.
3 U-GTG / Thrust Producing Gas Turbine Generators (60-70K LBS vertical thrust by themselves)
24 Graphene Based Super Conducting Lift Fans, 70-90K+ LBS vertically lift)
In the last image, for sizing comparison are
Discovery SSTO Heavy Lift: www.ioaircraft.com/hypersonic/discovery-218.php
Raven B Model, 22 Person Hypersonic Business Jet www.ioaircraft.com/hypersonic/raven-business.php
Grey Hawk, Mach 8-10 7th Gen Hypersonic Super Fighter www.ioaircraft.com/hypersonic/greyhawk.php
All are serial production ready.
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HVL130 VTOL Hypdersonic Transport Iteration 1 (vertical take off and landing)
HVL130 Condor, VTOL Hypersonic Transport, global point to point capable. www.ioaircraft.com/hypersonic/condor.php
130' length, 22-25 TON cargo bay capacity, H2 fueled, with onboard oxidizer as needed for Mach 15 velocity at 70 mile altitude (above the karman line). Website link: www.ioaircraft.com/hypersonic/condor.php
At apx 100,000-120,000ft, cruise velocity is Mach 8-10, with a 10,000nm range. Cargo bay and cockpit are hemetically sealed, with onboard oxygen supply and environmentals.
The entire cargo bay opens instead of a cargo bay door, while the nose gear retracts on the ground providing 8 1/2 ft of clearance into the bay.
*This same engineering principle that applies to Condor, can be scaled up further, with a 50-100 ton cargo capacity.
Propulsion for this aircraft is extensive:
2 U-TBCC (Unified Turbine Based Combine Cycle / Dual Mode Scramjet (300,000 LBS Thrust)
5 H2/O2 Compressed Fueled Bell Nozzle Rockets. No turbo pumps.
3 U-GTG / Thrust Producing Gas Turbine Generators (60-70K LBS vertical thrust by themselves)
24 Graphene Based Super Conducting Lift Fans, 70-90K+ LBS vertically lift)
In the last image, for sizing comparison are
Discovery SSTO Heavy Lift: www.ioaircraft.com/hypersonic/discovery-218.php
Raven B Model, 22 Person Hypersonic Business Jet www.ioaircraft.com/hypersonic/raven-business.php
Grey Hawk, Mach 8-10 7th Gen Hypersonic Super Fighter www.ioaircraft.com/hypersonic/greyhawk.php
All are serial production ready.
vtol, hypersonics, evtol, hydrogen, hsvtol, hypersonic, hypersonic plane, hypersonic aircraft, hypersonic jet, business jet, arrw, hsv, hawc, scramjet, tbcc, reaction engines, hermeus, hypersonix, hydrogen aviation, hydrogen aerospace, space plane, hypersonic weapons, icao, son of blackbird, scramjet physics, cfd, ramjet, supersonic, supersonic jet, aviation, aerospace, usaf, boeing, lockheed martin, northrop grumman, raytheon, turbine, dynetics, afrl, nrl, onr, defcon, darpa, graphene, physics, computational fluid dynamics, aircraft, nasa, engineering, energy, nsic AIAA, innovation, renewables, aerospace, green aerospace, AFWERX, Air Force Research Laboratory, United States Air Force, Defense Advanced Research Projects Agency, DARPA, NASA, National Aeronautics and Space Administration, Army Futures Command, USMC Special Operations, DLR, NATO