IO Aircraft
Raven SSTO - Iteration 12, Single Stage to Orbit - Space Plane (This is not a graphics design)
Raven SSTO - Iteration 12, Single Stage to Orbit - Space Plane (This is not a graphics design)
New iteration update, Raven SSTO, up to 15,000 LBS payloads to orbit for apx $2 mln per launch. Compresses O2 and H2 fueled, not liquid fueled. Graphene Airframe, 6,000+F thermal resistance. Air Breathing Aerospike, along with the primary U-TBCC propulsion.
Details at link www.ioaircraft.com/hypersonic/raven.php
Link to Raven www.ioaircraft.com/hypersonic/raven.php
Link to Discovery www.ioaircraft.com/hypersonic/discovery-218.php
Link to Conforming Tank Patent patents.google.com/patent/US20210080060
spaceplane, ssto, hypersonic, hypersonics, rocket, ksc, cape canaveral, space coast, space force, smallsat, orbital debris, satellite service, hydrogen, graphene, satellites, Space Tech, Reusable Rockets, Sustainable Space, RocketEngine, Spaceflight, darpa, air force research lab, afwerx, defwerx, nasa, aviation, airbus, engineering, defense, icao, aiaa, nro
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
Raven SSTO - Iteration 12, Single Stage to Orbit - Space Plane (This is not a graphics design)
Raven SSTO - Iteration 12, Single Stage to Orbit - Space Plane (This is not a graphics design)
New iteration update, Raven SSTO, up to 15,000 LBS payloads to orbit for apx $2 mln per launch. Compresses O2 and H2 fueled, not liquid fueled. Graphene Airframe, 6,000+F thermal resistance. Air Breathing Aerospike, along with the primary U-TBCC propulsion.
Details at link www.ioaircraft.com/hypersonic/raven.php
Link to Raven www.ioaircraft.com/hypersonic/raven.php
Link to Discovery www.ioaircraft.com/hypersonic/discovery-218.php
Link to Conforming Tank Patent patents.google.com/patent/US20210080060
spaceplane, ssto, hypersonic, hypersonics, rocket, ksc, cape canaveral, space coast, space force, smallsat, orbital debris, satellite service, hydrogen, graphene, satellites, Space Tech, Reusable Rockets, Sustainable Space, RocketEngine, Spaceflight, darpa, air force research lab, afwerx, defwerx, nasa, aviation, airbus, engineering, defense, icao, aiaa, nro
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