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The Space Launch System (SLS) core stage pathfinder, which is similar in similar in size, shape and weight to the 212-foot-tall core stage, arrived at NASA’s Michoud Assembly Facility early in the morning on September 27, 2017. To reduce the risk of first-time operations with one-of-a-kind spaceflight hardware for SLS, the agency built a core stage pathfinder. Like SLS, the core stage pathfinder will be doing something that's never been done -- testing new shipping and handling equipment and procedures from the manufacturing site to the test site to the launch site.
Image credit: NASA/MSFC/MAF/Steven Seipel
New iteration for Raven SSTO, Single Stage to Orbit. This isn't the heavy, Discovery. But the smaller one. For example, SpaceX's dragon capsule is 378 Cu Ft, Payload bay of Raven is 1078 Cu Ft. www.ioaircraft.com/hypersonic/raven.php
Iteration 10, almost clean sheet. U-TBCC propulsion, 6000F thermal resistance, 3D printed graphene airframe, Note the elimination of "blunt nose". Turn around time under 24 hours total from landing to ready for next flight. No external boosters.
Forward Thruster Bay, other then conventional orbital thrusters, also includes a reverse thruster which decelerates the aircraft pre re-entry into atmosphere from 16,500+ mph ground speed to apx 12,000 mph ground speed. Engines re-ignite once in atmosphere so it can fly to it's landing destination, ie not glide.
#ssto #singlestagetorobit #space #newspace #afrl #afwerx #usaf #darpa #onr #arl #boeing #lockheedmartin #raytheon #northropgrumman #aerojet #dynetics #esa #bae #afosr #hypersonics #hypersonic #scramjet #reactionengines #sabre #starship #falcon9 #dragoncapsule #innovation #graphene #hydrogen #spacex #ula #virginorbit #rocketlab #artemis #orion #sls #nasa #snc #sierranevadecorporation #dreamchaser #astra #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow
NASA Astronaut Anne McClain in LEGO brickheadz theme!
Maybe the best resemblance in my brickheadz so far. She's also a helicopter pilot. The Apollo Lunar Lander is said to have similarity with flying a helicopter. What will the Artemis lander be like? There are 3 different lander candidates now (Blue Origin, SpaceX, Dynetics).
Anne McClain's bio at NASA website:
www.nasa.gov/astronauts/biographies/anne-c-mcclain/biography
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NASAの月アルテミス計画のアン・マクレーン宇宙飛行士をレゴで作りました。これまでの自作Brickheadz Astronautzの中で一番似てるかも。
マクレーン飛行士はヘリコプターの操縦士でもあり、ヘリコプターはアポロ月面着陸船と操縦に共通点があるとか。アルテミス計画の着陸船はどんなデザインになるんでしょうね。候補は3つ(ブルーオリジン、スペースX、ダイネティクス社)に絞られているそうな。
NASA Astronaut Anne McClain in LEGO brickheadz theme!
Maybe the best resemblance in my brickheadz so far. She's also a helicopter pilot. The Apollo Lunar Lander is said to have similarity with flying a helicopter. What will the Artemis lander be like? There are 3 different lander candidates now (Blue Origin, SpaceX, Dynetics).
Anne McClain's bio at NASA website:
www.nasa.gov/astronauts/biographies/anne-c-mcclain/biography
.
.
NASAの月アルテミス計画のアン・マクレーン宇宙飛行士をレゴで作りました。これまでの自作Brickheadz Astronautzの中で一番似てるかも。
マクレーン飛行士はヘリコプターの操縦士でもあり、ヘリコプターはアポロ月面着陸船と操縦に共通点があるとか。アルテミス計画の着陸船はどんなデザインになるんでしょうね。候補は3つ(ブルーオリジン、スペースX、ダイネティクス社)に絞られているそうな。
Over at our strategic partner Dynetics’ facility, solid rocket booster separation shock testing was completed for our next-generation Vulcan Centaur rocket. Photo credit: United Launch Alliance
New iteration for Raven SSTO, Single Stage to Orbit. This isn't the heavy, Discovery. But the smaller one. For example, SpaceX's dragon capsule is 378 Cu Ft, Payload bay of Raven is 1078 Cu Ft. www.ioaircraft.com/hypersonic/raven.php
Iteration 10, almost clean sheet. U-TBCC propulsion, 6000F thermal resistance, 3D printed graphene airframe, Note the elimination of "blunt nose". Turn around time under 24 hours total from landing to ready for next flight. No external boosters.
Forward Thruster Bay, other then conventional orbital thrusters, also includes a reverse thruster which decelerates the aircraft pre re-entry into atmosphere from 16,500+ mph ground speed to apx 12,000 mph ground speed. Engines re-ignite once in atmosphere so it can fly to it's landing destination, ie not glide.
#ssto #singlestagetorobit #space #newspace #afrl #afwerx #usaf #darpa #onr #arl #boeing #lockheedmartin #raytheon #northropgrumman #aerojet #dynetics #esa #bae #afosr #hypersonics #hypersonic #scramjet #reactionengines #sabre #starship #falcon9 #dragoncapsule #innovation #graphene #hydrogen #spacex #ula #virginorbit #rocketlab #artemis #orion #sls #nasa #snc #sierranevadecorporation #dreamchaser #astra #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow
Iteration 10 - Raven B Model - Mach 8-10, 22 Passenger hypersonic business jet. New iteration reflects design changes from Raven A Model, which is an SSTO, a real one. ALL technologies associated "are" developed. It is also ZERO CARBON.
More Info: www.ioaircraft.com/hypersonic/raven-business.php
Not a graphics design or graphics rendering, but sanitized cad screenshots. This is not a concept, but ready for serial production. Not really looking for investors and such. Everything DOD is funding for hypersonic fixed aircraft is OLD and rehashed perpetually for 40+ years at 10X the price. Others, pushing supersonics and hypersonics, also very old technologies at very expensive prices and operating costs. This, about the same as a G650 or Global Express costs and operating costs and normalized Mach 10 dynamics in all regards in atmosphere.
#afrl #afwerx #defensewerx #usaf #darpa #onr #arl #boeing #lockheedmartin #airbus #raytheon #northropgrumman #aerojet #dynetics #easa #bae #afosr #hypersonic #supersonic #scramjet #reactionengines #innovation #graphene #hydrogen #spacex #ula #virgingalactic #rocketlab #nasa #snc #sierranevadecorporation #dreamchaser #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow #boomsuprsonic #aerion #esa #airplane
New iteration for Raven SSTO, Single Stage to Orbit. This isn't the heavy, Discovery. But the smaller one. For example, SpaceX's dragon capsule is 378 Cu Ft, Payload bay of Raven is 1078 Cu Ft. www.ioaircraft.com/hypersonic/raven.php
Iteration 10, almost clean sheet. U-TBCC propulsion, 6000F thermal resistance, 3D printed graphene airframe, Note the elimination of "blunt nose". Turn around time under 24 hours total from landing to ready for next flight. No external boosters.
Forward Thruster Bay, other then conventional orbital thrusters, also includes a reverse thruster which decelerates the aircraft pre re-entry into atmosphere from 16,500+ mph ground speed to apx 12,000 mph ground speed. Engines re-ignite once in atmosphere so it can fly to it's landing destination, ie not glide.
#ssto #singlestagetorobit #space #newspace #afrl #afwerx #usaf #darpa #onr #arl #boeing #lockheedmartin #raytheon #northropgrumman #aerojet #dynetics #esa #bae #afosr #hypersonics #hypersonic #scramjet #reactionengines #sabre #starship #falcon9 #dragoncapsule #innovation #graphene #hydrogen #spacex #ula #virginorbit #rocketlab #artemis #orion #sls #nasa #snc #sierranevadecorporation #dreamchaser #astra #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow
Secretary of the Army, Hon. Ryan D. McCarthy, visit's Northrup Gruman, Dynetics, and Army's Material Command HQ in Huntsville, AL., July. 1, 2020. (U.S. Army photo by Sgt. James Harvey)
Iteration 10 - Raven B Model - Mach 8-10, 22 Passenger hypersonic business jet. New iteration reflects design changes from Raven A Model, which is an SSTO, a real one. ALL technologies associated "are" developed. It is also ZERO CARBON.
More Info: www.ioaircraft.com/hypersonic/raven-business.php
Not a graphics design or graphics rendering, but sanitized cad screenshots. This is not a concept, but ready for serial production. Not really looking for investors and such. Everything DOD is funding for hypersonic fixed aircraft is OLD and rehashed perpetually for 40+ years at 10X the price. Others, pushing supersonics and hypersonics, also very old technologies at very expensive prices and operating costs. This, about the same as a G650 or Global Express costs and operating costs and normalized Mach 10 dynamics in all regards in atmosphere.
#afrl #afwerx #defensewerx #usaf #darpa #onr #arl #boeing #lockheedmartin #airbus #raytheon #northropgrumman #aerojet #dynetics #easa #bae #afosr #hypersonic #supersonic #scramjet #reactionengines #innovation #graphene #hydrogen #spacex #ula #virgingalactic #rocketlab #nasa #snc #sierranevadecorporation #dreamchaser #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow #boomsuprsonic #aerion #esa #airplane
19-050-3771DOE photo Lynn Freeny May29-30 2019 L to R Dr. David Burns NASA , Dr. Rebecca Ashford Chattanooga State, Dr. George Graham Wacker Polysilicon, Dr. Scott Smith ORNL, Kelly Jackson Dynetics May29-30 2019 Chattanooga Tennessee
Dynetics officially opened the Dr. Stephen M. Gilbert Advanced Manufacturing Facility on their campus in Huntsville's Cummings Research Park on May 30, 2019.
Secretary of the Army, Hon. Ryan D. McCarthy, visit's Northrup Gruman, Dynetics, and Army's Material Command HQ in Huntsville, AL., July. 1, 2020. (U.S. Army photo by Sgt. James Harvey)
New iteration for Raven SSTO, Single Stage to Orbit. This isn't the heavy, Discovery. But the smaller one. For example, SpaceX's dragon capsule is 378 Cu Ft, Payload bay of Raven is 1078 Cu Ft. www.ioaircraft.com/hypersonic/raven.php
Iteration 10, almost clean sheet. U-TBCC propulsion, 6000F thermal resistance, 3D printed graphene airframe, Note the elimination of "blunt nose". Turn around time under 24 hours total from landing to ready for next flight. No external boosters.
Forward Thruster Bay, other then conventional orbital thrusters, also includes a reverse thruster which decelerates the aircraft pre re-entry into atmosphere from 16,500+ mph ground speed to apx 12,000 mph ground speed. Engines re-ignite once in atmosphere so it can fly to it's landing destination, ie not glide.
#ssto #singlestagetorobit #space #newspace #afrl #afwerx #usaf #darpa #onr #arl #boeing #lockheedmartin #raytheon #northropgrumman #aerojet #dynetics #esa #bae #afosr #hypersonics #hypersonic #scramjet #reactionengines #sabre #starship #falcon9 #dragoncapsule #innovation #graphene #hydrogen #spacex #ula #virginorbit #rocketlab #artemis #orion #sls #nasa #snc #sierranevadecorporation #dreamchaser #astra #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow
Massive Ordnance Air Blast
The GBU-43/B MOAB (Massive Ordnance Air Blast) bomb, nicknamed “Mother Of All Bombs" is a large, powerful and accurately delivered high explosive weapon. The MOAB is the largest-ever satellite-guided, air-delivered weapon in history. The 21,600 lb MOAB is an improved replacement for the unguided 15,000 lb BLU-82 Daisy Cutter used in Vietnam and Afghanistan. MOAB is a guided bomb which delivers 18,700 lb of H6 explosive using a BLU-120/B warhead. It uses the KMU-593/B GPS/INS guidance system and is stabilized by series of fixed wings and grid (lattice) fins. The unique lattice fins offer excellent aerodynamic properties. It is designed to be launched from a C-130 aircraft, the MOAB is strapped to a specially designed cradle. Upon extraction from the aircraft the cradle is separated from the MOAB. The MOAB then proceeds to the target. The MOAB was developed, tested, and fielded by the Air Force Research Laboratory Munitions Directorate, Air Armament Center, the 46th Operations Group, Detachment 1 at Eglin AFB, FL in concert with other agencies and contractors. Within in ten months, the MOAB program went from development contract award to delivery into the Operational Theater. 26 February 2003 – First flight of inert weapon 07 March 2003 – Guided flight test of inert weapon displays capability of the massive “smart” bomb 11 March 2003 – Live flight test of the MOAB 11 April 2003 – Delivery of first MOAB into Operational Theater 13 April 2017 – First operational use of the MOAB in Afghanistan
Specifications
Manufacturer Air Force Research Laboratory/Dynetics, Inc.
Length 30 ft
Width 5 ft with fins retracted / 10 ft with fins extended
Diameter 40.5 in
Weight 21,600 lbs
Range Guided 3 nautical miles through a GPS system
Launch Platform MC-130 Talon II or “Slick” C-130 Aircraft
Armament 18,700 lbs of H6 Composition (1.35 times more powerful than TNT)
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
Iteration 10 - Raven B Model - Mach 8-10, 22 Passenger hypersonic business jet. New iteration reflects design changes from Raven A Model, which is an SSTO, a real one. ALL technologies associated "are" developed. It is also ZERO CARBON.
More Info: www.ioaircraft.com/hypersonic/raven-business.php
Not a graphics design or graphics rendering, but sanitized cad screenshots. This is not a concept, but ready for serial production. Not really looking for investors and such. Everything DOD is funding for hypersonic fixed aircraft is OLD and rehashed perpetually for 40+ years at 10X the price. Others, pushing supersonics and hypersonics, also very old technologies at very expensive prices and operating costs. This, about the same as a G650 or Global Express costs and operating costs and normalized Mach 10 dynamics in all regards in atmosphere.
#afrl #afwerx #defensewerx #usaf #darpa #onr #arl #boeing #lockheedmartin #airbus #raytheon #northropgrumman #aerojet #dynetics #easa #bae #afosr #hypersonic #supersonic #scramjet #reactionengines #innovation #graphene #hydrogen #spacex #ula #virgingalactic #rocketlab #nasa #snc #sierranevadecorporation #dreamchaser #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow #boomsuprsonic #aerion #esa #airplane
Iteration 10 - Raven B Model - Mach 8-10, 22 Passenger hypersonic business jet. New iteration reflects design changes from Raven A Model, which is an SSTO, a real one. ALL technologies associated "are" developed. It is also ZERO CARBON.
More Info: www.ioaircraft.com/hypersonic/raven-business.php
Not a graphics design or graphics rendering, but sanitized cad screenshots. This is not a concept, but ready for serial production. Not really looking for investors and such. Everything DOD is funding for hypersonic fixed aircraft is OLD and rehashed perpetually for 40+ years at 10X the price. Others, pushing supersonics and hypersonics, also very old technologies at very expensive prices and operating costs. This, about the same as a G650 or Global Express costs and operating costs and normalized Mach 10 dynamics in all regards in atmosphere.
#afrl #afwerx #defensewerx #usaf #darpa #onr #arl #boeing #lockheedmartin #airbus #raytheon #northropgrumman #aerojet #dynetics #easa #bae #afosr #hypersonic #supersonic #scramjet #reactionengines #innovation #graphene #hydrogen #spacex #ula #virgingalactic #rocketlab #nasa #snc #sierranevadecorporation #dreamchaser #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow #boomsuprsonic #aerion #esa #airplane
New iteration for Raven SSTO, Single Stage to Orbit. This isn't the heavy, Discovery. But the smaller one. For example, SpaceX's dragon capsule is 378 Cu Ft, Payload bay of Raven is 1078 Cu Ft. www.ioaircraft.com/hypersonic/raven.php
Iteration 10, almost clean sheet. U-TBCC propulsion, 6000F thermal resistance, 3D printed graphene airframe, Note the elimination of "blunt nose". Turn around time under 24 hours total from landing to ready for next flight. No external boosters.
Forward Thruster Bay, other then conventional orbital thrusters, also includes a reverse thruster which decelerates the aircraft pre re-entry into atmosphere from 16,500+ mph ground speed to apx 12,000 mph ground speed. Engines re-ignite once in atmosphere so it can fly to it's landing destination, ie not glide.
#ssto #singlestagetorobit #space #newspace #afrl #afwerx #usaf #darpa #onr #arl #boeing #lockheedmartin #raytheon #northropgrumman #aerojet #dynetics #esa #bae #afosr #hypersonics #hypersonic #scramjet #reactionengines #sabre #starship #falcon9 #dragoncapsule #innovation #graphene #hydrogen #spacex #ula #virginorbit #rocketlab #artemis #orion #sls #nasa #snc #sierranevadecorporation #dreamchaser #astra #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow
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
New iteration for Raven SSTO, Single Stage to Orbit. This isn't the heavy, Discovery. But the smaller one. For example, SpaceX's dragon capsule is 378 Cu Ft, Payload bay of Raven is 1078 Cu Ft. www.ioaircraft.com/hypersonic/raven.php
Iteration 10, almost clean sheet. U-TBCC propulsion, 6000F thermal resistance, 3D printed graphene airframe, Note the elimination of "blunt nose". Turn around time under 24 hours total from landing to ready for next flight. No external boosters.
Forward Thruster Bay, other then conventional orbital thrusters, also includes a reverse thruster which decelerates the aircraft pre re-entry into atmosphere from 16,500+ mph ground speed to apx 12,000 mph ground speed. Engines re-ignite once in atmosphere so it can fly to it's landing destination, ie not glide.
#ssto #singlestagetorobit #space #newspace #afrl #afwerx #usaf #darpa #onr #arl #boeing #lockheedmartin #raytheon #northropgrumman #aerojet #dynetics #esa #bae #afosr #hypersonics #hypersonic #scramjet #reactionengines #sabre #starship #falcon9 #dragoncapsule #innovation #graphene #hydrogen #spacex #ula #virginorbit #rocketlab #artemis #orion #sls #nasa #snc #sierranevadecorporation #dreamchaser #astra #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow
More info from Raven B Model - Iteration 10. Mach 8-10 Hypersonic Business Jet. Previous post lnkd.in/enxwifA was a new iteration update. Cleaning some things up, as I am not a graphics designer. Engineering, physics, etc yes. This post covers some technical aspects while still sanitizing everything.
For full size images, click thumbnail images on the website: www.ioaircraft.com/hypersonic/raven-business.php
Overall, this single aircraft design that is ready for building and going into serial production absolutely obliterates Lockheed's SR-72 (Mach 5) by DOUBLE the margins and a fraction of the costs, and BOOM, Virgin Galactic, etc.
Sure it can economically cruise at Mach 3-4.5 supersonically at under 50% throttle as well, but 7,000-8,000 NM Range at Mach 10 at over 100,000ft altitude and normalized hypersonic flight along with 6,000F thermal resistence.
A - Model is the SSTO (Single Stage to Orbit) version here: lnkd.in/efbmk_W
#afrl #afwerx #defensewerx #usaf #darpa #onr #arl #boeing #lockheedmartin #airbus #raytheon #northropgrumman #aerojet #dynetics #easa #bae #afosr #hypersonic #supersonic #scramjet #reactionengines #innovation #graphene #hydrogen #spacex #ula #virgingalactic #rocketlab #nasa #snc #sierranevadecorporation #dreamchaser #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow #boomsuprsonic #aerion #esa #easa #airplane
*Note, I use colors in my cad blocks and layer. I could easily tint/grey them out. I could care less how others do it. ALL dynamics are highly refined for normalized sustained Mach 10 flight. Extensive CFD refinement over many years, along with material science, and several upcoming patent filings for individual technology advancements, along with 2nd gen high pressure conforming tanks that utilize graphene inner shells at 2,000,000 PSI tensile strength normalizing 16,000 PSI high pressure storage vessels. Everything else is already developed as well.
hypersonic plane, supersonic plane, supersonic private jet, hypersonic private jet, afrl, afwerx, defensewerx, usaf, darpa, onr, arl, boeing, lockheed martin, airbus, raytheon, northrop grumman, aerojet, dynetics, easa, bae, afosr, hypersonic, supersonic, scramjet, reaction engines, innovation, graphene, hydrogen, spacex, ula, virgin galactic, rocketlab, nasa, snc, sierra nevade corporation, dream chaser, sdo, sda, space force, dod, icao, dassault, bombardier, gulfstream, cessna, bigalow, boom suprsonic, aerion, tbcc, mayhem
Iteration 10 - Raven B Model - Mach 8-10, 22 Passenger hypersonic business jet. New iteration reflects design changes from Raven A Model, which is an SSTO, a real one. ALL technologies associated "are" developed. It is also ZERO CARBON.
More Info: www.ioaircraft.com/hypersonic/raven-business.php
Not a graphics design or graphics rendering, but sanitized cad screenshots. This is not a concept, but ready for serial production. Not really looking for investors and such. Everything DOD is funding for hypersonic fixed aircraft is OLD and rehashed perpetually for 40+ years at 10X the price. Others, pushing supersonics and hypersonics, also very old technologies at very expensive prices and operating costs. This, about the same as a G650 or Global Express costs and operating costs and normalized Mach 10 dynamics in all regards in atmosphere.
#afrl #afwerx #defensewerx #usaf #darpa #onr #arl #boeing #lockheedmartin #airbus #raytheon #northropgrumman #aerojet #dynetics #easa #bae #afosr #hypersonic #supersonic #scramjet #reactionengines #innovation #graphene #hydrogen #spacex #ula #virgingalactic #rocketlab #nasa #snc #sierranevadecorporation #dreamchaser #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow #boomsuprsonic #aerion #esa #airplane
More info from Raven B Model - Iteration 10. Mach 8-10 Hypersonic Business Jet. Previous post lnkd.in/enxwifA was a new iteration update. Cleaning some things up, as I am not a graphics designer. Engineering, physics, etc yes. This post covers some technical aspects while still sanitizing everything.
For full size images, click thumbnail images on the website: www.ioaircraft.com/hypersonic/raven-business.php
Overall, this single aircraft design that is ready for building and going into serial production absolutely obliterates Lockheed's SR-72 (Mach 5) by DOUBLE the margins and a fraction of the costs, and BOOM, Virgin Galactic, etc.
Sure it can economically cruise at Mach 3-4.5 supersonically at under 50% throttle as well, but 7,000-8,000 NM Range at Mach 10 at over 100,000ft altitude and normalized hypersonic flight along with 6,000F thermal resistence.
A - Model is the SSTO (Single Stage to Orbit) version here: lnkd.in/efbmk_W
#afrl #afwerx #defensewerx #usaf #darpa #onr #arl #boeing #lockheedmartin #airbus #raytheon #northropgrumman #aerojet #dynetics #easa #bae #afosr #hypersonic #supersonic #scramjet #reactionengines #innovation #graphene #hydrogen #spacex #ula #virgingalactic #rocketlab #nasa #snc #sierranevadecorporation #dreamchaser #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow #boomsuprsonic #aerion #esa #easa #airplane
*Note, I use colors in my cad blocks and layer. I could easily tint/grey them out. I could care less how others do it. ALL dynamics are highly refined for normalized sustained Mach 10 flight. Extensive CFD refinement over many years, along with material science, and several upcoming patent filings for individual technology advancements, along with 2nd gen high pressure conforming tanks that utilize graphene inner shells at 2,000,000 PSI tensile strength normalizing 16,000 PSI high pressure storage vessels. Everything else is already developed as well.
hypersonic plane, supersonic plane, supersonic private jet, hypersonic private jet, afrl, afwerx, defensewerx, usaf, darpa, onr, arl, boeing, lockheed martin, airbus, raytheon, northrop grumman, aerojet, dynetics, easa, bae, afosr, hypersonic, supersonic, scramjet, reaction engines, innovation, graphene, hydrogen, spacex, ula, virgin galactic, rocketlab, nasa, snc, sierra nevade corporation, dream chaser, sdo, sda, space force, dod, icao, dassault, bombardier, gulfstream, cessna, bigalow, boom suprsonic, aerion, tbcc, mayhem
More info from Raven B Model - Iteration 10. Mach 8-10 Hypersonic Business Jet. Previous post lnkd.in/enxwifA was a new iteration update. Cleaning some things up, as I am not a graphics designer. Engineering, physics, etc yes. This post covers some technical aspects while still sanitizing everything.
For full size images, click thumbnail images on the website: www.ioaircraft.com/hypersonic/raven-business.php
Overall, this single aircraft design that is ready for building and going into serial production absolutely obliterates Lockheed's SR-72 (Mach 5) by DOUBLE the margins and a fraction of the costs, and BOOM, Virgin Galactic, etc.
Sure it can economically cruise at Mach 3-4.5 supersonically at under 50% throttle as well, but 7,000-8,000 NM Range at Mach 10 at over 100,000ft altitude and normalized hypersonic flight along with 6,000F thermal resistence.
A - Model is the SSTO (Single Stage to Orbit) version here: lnkd.in/efbmk_W
#afrl #afwerx #defensewerx #usaf #darpa #onr #arl #boeing #lockheedmartin #airbus #raytheon #northropgrumman #aerojet #dynetics #easa #bae #afosr #hypersonic #supersonic #scramjet #reactionengines #innovation #graphene #hydrogen #spacex #ula #virgingalactic #rocketlab #nasa #snc #sierranevadecorporation #dreamchaser #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow #boomsuprsonic #aerion #esa #easa #airplane
*Note, I use colors in my cad blocks and layer. I could easily tint/grey them out. I could care less how others do it. ALL dynamics are highly refined for normalized sustained Mach 10 flight. Extensive CFD refinement over many years, along with material science, and several upcoming patent filings for individual technology advancements, along with 2nd gen high pressure conforming tanks that utilize graphene inner shells at 2,000,000 PSI tensile strength normalizing 16,000 PSI high pressure storage vessels. Everything else is already developed as well.
hypersonic plane, supersonic plane, supersonic private jet, hypersonic private jet, afrl, afwerx, defensewerx, usaf, darpa, onr, arl, boeing, lockheed martin, airbus, raytheon, northrop grumman, aerojet, dynetics, easa, bae, afosr, hypersonic, supersonic, scramjet, reaction engines, innovation, graphene, hydrogen, spacex, ula, virgin galactic, rocketlab, nasa, snc, sierra nevade corporation, dream chaser, sdo, sda, space force, dod, icao, dassault, bombardier, gulfstream, cessna, bigalow, boom suprsonic, aerion, tbcc, mayhem
Iteration 10 - Raven B Model - Mach 8-10, 22 Passenger hypersonic business jet. New iteration reflects design changes from Raven A Model, which is an SSTO, a real one. ALL technologies associated "are" developed. It is also ZERO CARBON.
More Info: www.ioaircraft.com/hypersonic/raven-business.php
Not a graphics design or graphics rendering, but sanitized cad screenshots. This is not a concept, but ready for serial production. Not really looking for investors and such. Everything DOD is funding for hypersonic fixed aircraft is OLD and rehashed perpetually for 40+ years at 10X the price. Others, pushing supersonics and hypersonics, also very old technologies at very expensive prices and operating costs. This, about the same as a G650 or Global Express costs and operating costs and normalized Mach 10 dynamics in all regards in atmosphere.
#afrl #afwerx #defensewerx #usaf #darpa #onr #arl #boeing #lockheedmartin #airbus #raytheon #northropgrumman #aerojet #dynetics #easa #bae #afosr #hypersonic #supersonic #scramjet #reactionengines #innovation #graphene #hydrogen #spacex #ula #virgingalactic #rocketlab #nasa #snc #sierranevadecorporation #dreamchaser #sdo #sda #spaceforce #dod #icao #dassault #bombardier #gulfstream #cessna #bigalow #boomsuprsonic #aerion #esa #airplane
Dynetics officially opened the Dr. Stephen M. Gilbert Advanced Manufacturing Facility on their campus in Huntsville's Cummings Research Park on May 30, 2019.
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
Dynetics officially opened the Dr. Stephen M. Gilbert Advanced Manufacturing Facility on their campus in Huntsville's Cummings Research Park on May 30, 2019.
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
Massive Ordnance Air Blast
The GBU-43/B MOAB (Massive Ordnance Air Blast) bomb, nicknamed “Mother Of All Bombs" is a large, powerful and accurately delivered high explosive weapon. The MOAB is the largest-ever satellite-guided, air-delivered weapon in history. The 21,600 lb MOAB is an improved replacement for the unguided 15,000 lb BLU-82 Daisy Cutter used in Vietnam and Afghanistan. MOAB is a guided bomb which delivers 18,700 lb of H6 explosive using a BLU-120/B warhead. It uses the KMU-593/B GPS/INS guidance system and is stabilized by series of fixed wings and grid (lattice) fins. The unique lattice fins offer excellent aerodynamic properties. It is designed to be launched from a C-130 aircraft, the MOAB is strapped to a specially designed cradle. Upon extraction from the aircraft the cradle is separated from the MOAB. The MOAB then proceeds to the target. The MOAB was developed, tested, and fielded by the Air Force Research Laboratory Munitions Directorate, Air Armament Center, the 46th Operations Group, Detachment 1 at Eglin AFB, FL in concert with other agencies and contractors. Within in ten months, the MOAB program went from development contract award to delivery into the Operational Theater. 26 February 2003 – First flight of inert weapon 07 March 2003 – Guided flight test of inert weapon displays capability of the massive “smart” bomb 11 March 2003 – Live flight test of the MOAB 11 April 2003 – Delivery of first MOAB into Operational Theater 13 April 2017 – First operational use of the MOAB in Afghanistan
Specifications
Manufacturer Air Force Research Laboratory/Dynetics, Inc.
Length 30 ft
Width 5 ft with fins retracted / 10 ft with fins extended
Diameter 40.5 in
Weight 21,600 lbs
Range Guided 3 nautical miles through a GPS system
Launch Platform MC-130 Talon II or “Slick” C-130 Aircraft
Armament 18,700 lbs of H6 Composition (1.35 times more powerful than TNT)
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
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
Dynetics officially opened the Dr. Stephen M. Gilbert Advanced Manufacturing Facility on their campus in Huntsville's Cummings Research Park on May 30, 2019.
Secretary of the Army, Hon. Ryan D. McCarthy, visit's Northrup Gruman, Dynetics, and Army's Material Command HQ in Huntsville, AL., July. 1, 2020. (U.S. Army photo by Sgt. James Harvey)
Secretary of the Army, Hon. Ryan D. McCarthy, visit's Northrup Gruman, Dynetics, and Army's Material Command HQ in Huntsville, AL., July. 1, 2020. (U.S. Army photo by Sgt. James Harvey)
Interoperability among all Army UAS assets is a key element of MUM-T. Here, Interoperability Engineer David Campbell, a contractor with Dynetics, works on AIC testing of the Gray Eagle and Apache Block III at JSIL, Redstone Arsenal, AL. (U.S. Army photo courtesy of PM UAS)
Secretary of the Army, Hon. Ryan D. McCarthy, visit's Northrup Gruman, Dynetics, and Army's Material Command HQ in Huntsville, AL., July. 1, 2020. (U.S. Army photo by Sgt. James Harvey)
John Coogan (right), a recent master's graduate from the school of Mechanical & Aerospace Engineering and Graduate Research Assistant with the PRC, is now employed with Dynetics, Inc. in Huntsville. He will be moving to Charlottesville, VA to provide on-site engineering support to the US Army. He is shown here with his academic adviser, Dr. Nathan SLegers (left).
Secretary of the Army, Hon. Ryan D. McCarthy, visit's Northrup Gruman, Dynetics, and Army's Material Command HQ in Huntsville, AL., July. 1, 2020. (U.S. Army photo by Sgt. James Harvey)
Secretary of the Army, Hon. Ryan D. McCarthy, visit's Northrup Gruman, Dynetics, and Army's Material Command HQ in Huntsville, AL., July. 1, 2020. (U.S. Army photo by Sgt. James Harvey)
Secretary of the Army, Hon. Ryan D. McCarthy, visit's Northrup Gruman, Dynetics, and Army's Material Command HQ in Huntsville, AL., July. 1, 2020. (U.S. Army photo by Sgt. James Harvey)
Secretary of the Army, Hon. Ryan D. McCarthy, visit's Northrup Gruman, Dynetics, and Army's Material Command HQ in Huntsville, AL., July. 1, 2020. (U.S. Army photo by Sgt. James Harvey)