IO Aircraft - Hyperion C - Mach 15 Scramjet Missile

Hyperion C - Mach 15 Scramjet Platform With Super Conducting Plasma Actuation

Total Length:	110"
Wingspan: Booster Dia Payload Weight	20" 22" Optional 122 LBS Steel Weight Minus Boosters, Apx 200 LBS (X-51 1,228 LBS)
Propulsion	Variable Geometry Mach 15 Scramjet

Fuel:	Hydrogen (16,000 PSI) 17 Gallons, equivalent to 68 Gallons at 4,000 PSI
Range	1,000 NM Under Power 1,000+ NM Range Coast Total Range, 2,000-3,000 NM
Estimated Production Cost	$1.2 Million in Production

Hyperion C, is the 3rd generation of the Hyperion Series for Mach 10-15 Scramjet capabilities.

Hyperion C is a clean sheet design, physics, and engineering incorporating the most advanced technologies for hypersonic capabilities in existence.

Fuel for this platform is compressed hydrogen, utilizing our own 2nd gen high pressure conforming tank technologies which are patented by USPTO US20210080060 which allows this platform to have a 17 gallons capacity (3,927 cubic inch) at 16,000 PSI. This pressure is the equivalent to 68 gallons at a standard high pressure cylinder volume. This allows us to store 400% more energy, but because this is a conforming tank, cylinders no longer matter, we can produce them in any overall shap to conforming with the aerospace/product dimensions.

The propulsion for Hyperion B is a very advanced scramjet with dynamic fuel/air mixture and dynamic ignition, which allow for much high performance for scramjet propulsion and self start.

The variable geometry aspects for the inlet decks, also provides for a broad envelope for operating anywhere from Mach 10-15 and from 30,000ft to 90,000+ ft, which no scramjet produced to date is able to operate. Lower altitude capabilities for Hyperion C, are un-attainable by any defense funded program in existence, due to aerothermaldynamics.

But we eliminate this by incorporated Superconducting Plasma Actuation, also commonly referred to as Dielectric Laminar Flow Control. Except ours is much more advanced, providing greater then 1,000% the actuation effects vs any funded program.

Superconducting plasma actuation, allow Hyperion C to produce a plasma shield around the BOW region of the aircraft, thus minimal thermal transfer occurs resulting in surface temps of only 200-500F, rather then 3,000+F at Mach 10.

Additionally, this plasma shield is controllable and offers attitude control of the nose of the aircraft, enhanced control authority. These same features are built into the ventral ducts offer enhanced roll and elevator control as well.

Hyperion C's fuselage and under skin is 3D printed graphene, as 1 single piece. Because of this, the airframe itself weighs only a few pounds, but the strength is 33X greater then solid titanium. After all hardware and systems are installed, total weight of the platform itself is approximately 200 LBS. To put that into comparison, the X-51 was 1,228 LBS. HAWC, etc are similar heavier weights.

Because of this light weight, the fuel consumption is much less to other scramjet propelled platforms, which results in much longer endurance under power. Just to increase the kinetic energy further for impact, a 122 LBS steel ballast weight can be added.

Super Conducting Plasma Actuation, dielectric plasma actuation, Hypersonic UCAV, Hypersonic UAV, vtol hypersonics, Hypersonic Aircraft, Hypersonic Jet, IO Aircraft, scramjet, ramjet, turbine based combined cycle, glide breaker, hypersonic, hypersonic weapon, hypersonic missile, Air Launched Rapid Response Weapon, ARRW, scramjet missile, boost glide, tactical glide vehicle, phantom works, skunk works, htv, hypersonic tactical vehicle, afrl, onr, hacm, boeing, utc, utx, ge, TBCC, RBCC, Reaction Engines, plane, turbine, spacex, virgin orbit, virgin galactic, usaf, single stage to orbit, sto, space plane, falcon heavy, delta iv, hypersonic commercial aircraft, hypersonic commercial plane, hypersonic aircraft, hypersonic plane, ICAO, boeing phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet engineering, scramjet physics, scramjet, ramjet, dual mode ramjet, darpa, onr, navair, afrl, aerion supersonic, aerion, spike aerospace, boom supersonic, air taxi, vtol, personal air vehicle, vertical take off and landing, urban air mobility, ultralight, far 103, experimental, type certified, dual mode ramjet, scramjet engineering, scramjet physics, hypersonic weapons, hypersonic missiles, boost glide, tactical glide vehicle, phantom express, xs-1, htv, Air-Launched Rapid Response Weapon, ARRW, hypersonic tactical vehicle

Hypersonic Plane, Hypersonic Aircraft, Hypersonic Jet, IO Aircraft, scramjet, ramjet, turbine based combined cycle, glide breaker, hypersonic, hypersonic weapon, hypersonic missile, Air Launched Rapid Response Weapon, ARRW, scramjet missile, boost glide, tactical glide vehicle, phantom works, skunk works, htv, hypersonic tactical vehicle, afrl, onr, boeing, utc, utx, ge, TBCC, RBCC, Reaction Engines, plane, turbine, spacex, virgin orbit, virgin galactic, usaf, single stage to orbit, sto, space plane, falcon heavy, delta iv, hypersonic commercial aircraft, hypersonic commercial plane, hypersonic aircraft, hypersonic plane, ICAO, boeing phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet engineering, scramjet physics, scramjet, ramjet, dual mode ramjet, darpa, onr, navair, afrl, aerion supersonic, aerion, spike aerospace, boom supersonic, air taxi, vtol, personal air vehicle, vertical take off and landing, urban air mobility, ultralight, far 103, experimental, type certified, dual mode ramjet, scramjet engineering, scramjet physics, hypersonic weapons, hypersonic missiles, boost glide, tactical glide vehicle, phantom express, xs-1, htv, Air-Launched Rapid Response Weapon, ARRW, hypersonic tactical vehicle