View allAll Photos Tagged fighterplane
A Lockheed Martin F-35 Lightning II belonging to the Royal Netherlands Air Force on the static display at the 2022 Abbotsford Airshow.
A USAF F-15 Eagle flying during the evening show of the 2022 Abbotsford Airshow. Thanks to it being an evening show, I got some good shots of the Eagle's afterburners.
A US Navy E/A18G Growler flying during the Growler demo at the 2025 Abbotsford Airshow. It was loud and the pilots didn't hold back. I can still hear the afterburners when I look at these shots.
The Supermarine Spitfire, bred from the Schneider Trophy winning seaplane racers of the 30s, an incredibly elegant, agile and fast fighter, triumph of design and engineering. But oh so much more than that in the collective psyche of these islands, the Spit is forever associated with that moment when the history of the free world balanced on a knife edge, the Battle of Britain, and remains for many of us a supreme symbol of defiance against the odds in the face of overwhelming evil which had swallowed so much else but found the RAF more than they could chew...
This Spit was constructed late in the war, 1944, so long after that watershed air battle, although in the 1960s she would be taking to the air for part of the movie Battle of Britain. She's been the 'gate guard' at various RAF bases, including Leuchars, over the years and was eventually donated to the city of Glasgow (she had once been part of the City of Glasgow auxiliary RAF squadron in her history), refurbished at the National Museum of Flight at East Fortune and when the magnificent Kelvingrove Art Gallery & Museum re-opened after a huge redevelopment she was on display, hanging there amid the early 1900s architecture, rather delightfully right over the head of a stuffed giraffe on display with other animals below! There's something quite magical about turning into a wing of this huge, historic edifice and coming face to face with a real Spitfire just hanging there, the lines so elegant and aerodynamic she still looks fast even when hanging still...
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️ eXploration (1) West Coast {USA}
🌟 West Coast {USA}
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📝 Type : Ground eXploration
🎨 Style : eXploration of the west coast of the united states
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❓ WHY : To eXplore the west coast of the united states
📍 WHERE : West Coast (🇺🇸 United States of America)
🕓 WHEN : 12 June 2011
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PictionID:42253585 - Title:Lockheed F-104G cn 4013 61-2613 141st Sqd Turkish AF (Jelle Sjoerdsma via RJF) - Catalog:17_000026 - Filename:17_000026.tif - ---------Image from the René Francillon Photo Archive. Having had his interest in aviation sparked by being at the receiving end of B-24s bombing occupied France when he was 7-yr old, René Francillon turned aviation into both his vocation and avocation. Most of his professional career was in the United States, working for major aircraft manufacturers and airport planning/design companies. All along, he kept developing a second career as an aviation historian, an activity that led him to author more than 50 books and 400 articles published in the United States, the United Kingdom, France, and elsewhere. Far from “hanging on his spurs,” he plans to remain active as an author well into his eighties.-------PLEASE TAG this image with any information you know about it, so that we can permanently store this data with the original image file in our Digital Asset Management System.--------------SOURCE INSTITUTION: San Diego Air and Space Museum Archive
Recovered on a mountain top in New Guinea this P-61 is currently undergoing restoration at the Mid-Atlantic Air Museum in Reading, PA. Upon completion it will be one of four left and the only one in flight condition.
Captured Sunday at the CNE Air Show. This airplane put on an incredible show and was unbelievably hard to capture. The above image is the plane just before it rolls over at full throttle(?) In the next image I was lucky enough to capture the Raptor directly in the middle of the back roll and I swear you can see the flex of the plane. I'll upload the 'F-22 Flexing' image next.
The Lockheed Martin/Boeing F-22 Raptor is a fifth-generation fighter aircraft that uses stealth technology. It was designed primarily as an air superiority fighter, but has additional capabilities that include ground attack, electronic warfare, and signals intelligence roles. Lockheed Martin Aeronautics is the prime contractor and is responsible for the majority of the airframe, weapon systems and final assembly of the F-22. Program partner Boeing Integrated Defense Systems provides the wings, aft fuselage, avionics integration, and all of the pilot and maintenance training systems.
The aircraft was variously designated F-22 and F/A-22 during the years prior to formally entering USAF service in December 2005 as the F-22A. Despite a protracted and costly development period, the United States Air Force considers the F-22 a critical component for the future of US tactical airpower, and claims that the aircraft is unmatched by any known or projected fighter,[3] while Lockheed Martin claims that the Raptor's combination of stealth, speed, agility, precision and situational awareness, combined with air-to-air and air-to-ground combat capabilities, makes it the best overall fighter in the world.[7] Air Chief Marshal Angus Houston, Chief of the Australian Defence Force, said in 2004 that the "F-22 will be the most outstanding fighter plane ever built."[8] In April 2009 the US Department of Defense proposed to cease placing new orders, subject to Congressional approval, for a final procurement tally of 187 Raptors.[9] The US Senate and House each passed 2010 budget bill versions without F-22 production funding in July 2009.[10] Congress will combine these versions into one bill for presidential approval
Raven - Model B Mach 8-10 - Supersonic / Hypersonic Business Jet - Iteration 6
Seating: 22 | Crew 2+1
Length: 100ft | Span: 45ft 8in
Engines: 2 U-TBCC (Unified Turbine Based Combined Cycle)
Fuel: H2 (Compressed Hydrogen)
Cruising Altitude: 100,000-125,000 ft @ Mach 8-10
Air frame: 75% Proprietary Composites
Operating Costs, Similar to the hourly operating costs of a Gulfstream G650 or Bombardier Global Express 7000 Series
IO Aircraft www.ioaircraft.com
Drew Blair www.linkedin.com/in/drew-b-25485312/
-----------------------------
supersonic business jet, hypersonic business jet, hypersonic plane, hypersonic aircraft, hypersonic commercial plane, hypersonic commercial aircraft, hypersonic airline, Aerion, Aerion Supersonic, tbcc, glide breaker, fighter plane, hyperonic fighter, boeing phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, office of naval research, defense advanced research project agency, defense science, missile defense agency, aerospike, hydrogen, hydrogen storage, hydrogen fueled, hydrogen aircraft, virgin airlines, united airlines, sas, finnair ,emirates airlines, ANA, JAL, airlines, military, physics, airline, british airways, air france
-----------------------------
Unified Turbine Based Combined Cycle. Current technologies and what Lockheed is trying to force on the Dept of Defense, for that low speed Mach 5 plane DOD gave them $1 billion to build and would disintegrate above Mach 5, is TBCC. 2 separate propulsion systems in the same airframe, which requires TWICE the airframe space to use.
Unified Turbine Based Combined Cycle is 1 propulsion system cutting that airframe deficit in half, and also able to operate above Mach 10 up to Mach 15 in atmosphere, and a simple nozzle modification allows for outside atmosphere rocket mode, ie orbital capable.
Additionally, Reaction Engines maximum air breather mode is Mach 4.5, above that it will explode in flight from internal pressures are too high to operate. Thus, must switch to non air breather rocket mode to operate in atmosphere in hypersonic velocities. Which as a result, makes it not feasible for anything practical. It also takes an immense amount of fuel to function.
-------------
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
'N3290' Is a replica. The original having been shot down over France in May 1940. It's pilot survived & spent the remainder of the war as a P.O.W.
This aircraft is visiting Arley station, as part of the Severn Valley Railway's 1940's weekend.
Construction of these fighters started in 1923, and a few dozen only seem to have been ordered. By 1930, they were assigned to a Marine Fighter Squad.
A 520 HP 12-cyl Packard engine gave the FB-5 all of 282 km/h (175 mph) top speed. They were armed with two .30 Browning machine guns.
This sopwith camel fighter plane, flown by one of Snoopy's alter egos, was designed and built by airplane hobbyist, Jack Williams of Rice Lake, Wisconsin in 1978. On May 12, 2001, he donated it to the Snoopy Gallery and Gift Shop in Memory of Charles Schulz.
Snoopy first appeared as the World War I Flying Ace in October, 1965. Since then the adventures of the fictional dog chasing the famous German ace pilot, Baron Von Richthoven, have filled comic pages and television screens.
Snoopy's Gallery & Gift Shop, located next to the Redwood Empire Ice Arena at 1665 West Steele Lane in Santa Rosa, features 2,400 square feet of a wide range of Peanuts products.
70 Ton Payload, Single Stage to Orbit Fixed Wing Aircraft - Hypersonic Plane - Space Plane
Earlier, pre Iteration 1, Just felt like posting this online, working out the physics/geometries/energy requirements and contruction.
Mach 8-10 in amtmosphere, 195ft long, Heavy Lift Single Stage To Orbit Fixed Wing Aircraft. 70 TONS, ie 140,000 LBS, 60 ft X 15ft X 15ft payload bay. Up in the Falcon Heavy and Delta IV class, except not $400 million to launch giant payloads into orbit, but below $250 per lbs, or about $28 million to launch giant payloads, and normalized orbital flight, as normal as a 737 commercial flight. Load up, refuel, take off in an afternoon. I estimate this aircraft would cost about $750 million each for space capable. In atmosphere commercial, roughly $300 million each for a 200 passenger M8-10 (not designed yet)
--------------
www.ioaircraft.com/hypersonic/ranger.php
Drew Blair
www.linkedin.com/in/drew-b-25485312/
--------------
Unified Turbine Based Combined Cycle. Current technologies and what Lockheed is trying to force on the Dept of Defense, for that low speed Mach 5 plane DOD gave them $1 billion to build and would disintegrate above Mach 5, is TBCC. 2 separate propulsion systems in the same airframe, which requires TWICE the airframe space to use.
Unified Turbine Based Combined Cycle is 1 propulsion system cutting that airframe deficit in half, and also able to operate above Mach 10 up to Mach 15 in atmosphere, and a simple nozzle modification allows for outside atmosphere rocket mode, ie orbital capable.
Additionally, Reaction Engines maximum air breather mode is Mach 4.5, above that it will explode in flight from internal pressures are too high to operate. Thus, must switch to non air breather rocket mode to operate in atmosphere in hypersonic velocities. Which as a result, makes it not feasible for anything practical. It also takes an immense amount of fuel to function.
-------------
tbcc, glide breaker, fighter plane, hyperonic fighter, stealth fighter, boeing phantom express, phantom works, boeing phantom works, lockheed skunk works, hypersonic weapon, hypersonic missile, scramjet missile, scramjet engineering, scramjet physics, boost glide, tactical glide vehicle, Boeing XS-1, htv, Air Launched Rapid Response Weapon, (ARRW), hypersonic tactical vehicle, hypersonic plane, hypersonic aircraft, space plane, scramjet, turbine based combined cycle, ramjet, dual mode ramjet, darpa, onr, navair, afrl, air force research lab, office of naval research, defense advanced research project agency, defense science, missile defense agency, aerospike, vtol, vertical take off, air taxi, personal air vehicle, boeing go fly prize, go fly prize,
Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
Creator: Unidentified.
Location: Moreton Bay, Queensland.
Description: Final test flight of a P-38 Lightning over Moreton Bay, southern Queensland. (Information taken from: 81st Air Depot Group, 5th Air Force, USAAF in Australia during World War II, 2002, retrieved 17 February 2003, from ).
The Lockheed P-38 Lightning was simply the most versatile aircraft used in World War II. After a lengthy developmental period, the P-38 eventually flourished in multiple roles. In its designed role, the P-38 was an effective fighter and was the main aircraft for most of the aces in the Pacific Theater of Operations. (Information taken from: P-38 Lightning Online, 2003, retrieved 17 February 2003, from ).
View the original image at the State Library of Queensland: hdl.handle.net/10462/deriv/112266.
Information about State Library of Queensland’s collection: www.slq.qld.gov.au/research-collections.
You are free to use this image without permission. Please attribute State Library of Queensland.
The Sanicole Airshow.
The yearly amazingness in Belgium on September 10 and 11 2022 has passed.
It was, as each year, an early start for me on Sunday morning, September 11th, to visit the yearly Sanicole Airshow.
Saturday's Sunset show has been fantastic according to the messages on social media channels. Unfortunately, the weather was a bit less enthusiastic.
The warning for Sunday was to bring suitable waterproof footwear and clothing to the show.
So I did.
Friend of Sanicole
This year I decided to do it a little bit different than the previous years.
Instead of standing on the field, I bought tickets for the stand.
Here you have the opportunity to sit and besides that, you can see the whole terrain. Another plus is that drinks are included for the whole day!
Obviously, that's a bit more relaxed than standing on your feet for the whole day and bringing your own seats, food and drinks. (food and drinks are not cheap during these events of course)
Sunday, September 11th 2022
The weather was starting the wrong way, unfortunately.
The fog was everywhere from my home to the airshow field.
In the end, the show started about an hour and a half later than planned.
I was surrounded by some aviation-enthusiastic German people.
They had a funny way of having their breakfast. Some booze and soda. Good start but funny to watch.
Anyways, it was all worth waiting for the show when it finally started.
Because, this year we had, for me, new demo teams.
There
A US Navy E/A18G Growler flying during the Growler demo at the 2025 Abbotsford Airshow. It was loud and the pilots didn't hold back. I can still hear the afterburners when I look at these shots.
F-15E Strike Eagle just landed at RAF Lakenheath this morning. RAF lakenheath in Suffolk UK is home to the USAF 48th Fighter Wing, The Statue of Liberty Wing.
Raven - Model B Mach 8-10 - Supersonic / Hypersonic Business Jet - Iteration 6
Seating: 22 | Crew 2+1
Length: 100ft | Span: 45ft 8in
Engines: 2 U-TBCC (Unified Turbine Based Combined Cycle)
Fuel: H2 (Compressed Hydrogen)
Cruising Altitude: 100,000-125,000 ft @ Mach 8-10
Air frame: 75% Proprietary Composites
Operating Costs, Similar to the hourly operating costs of a Gulfstream G650 or Bombardier Global Express 7000 Series
IO Aircraft www.ioaircraft.com
Drew Blair www.linkedin.com/in/drew-b-25485312/
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Unified Turbine Based Combined Cycle. Current technologies and what Lockheed is trying to force on the Dept of Defense, for that low speed Mach 5 plane DOD gave them $1 billion to build and would disintegrate above Mach 5, is TBCC. 2 separate propulsion systems in the same airframe, which requires TWICE the airframe space to use.
Unified Turbine Based Combined Cycle is 1 propulsion system cutting that airframe deficit in half, and also able to operate above Mach 10 up to Mach 15 in atmosphere, and a simple nozzle modification allows for outside atmosphere rocket mode, ie orbital capable.
Additionally, Reaction Engines maximum air breather mode is Mach 4.5, above that it will explode in flight from internal pressures are too high to operate. Thus, must switch to non air breather rocket mode to operate in atmosphere in hypersonic velocities. Which as a result, makes it not feasible for anything practical. It also takes an immense amount of fuel to function.
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Advanced Additive Manufacturing for Hypersonic Aircraft
Utilizing new methods of fabrication and construction, make it possible to use additive manufacturing, dramatically reducing the time and costs of producing hypersonic platforms from missiles, aircraft, and space capable craft. Instead of aircraft being produced in piece, then bolted together; small platforms can be produced as a single unit and large platforms can be produces in large section and mated without bolting. These techniques include using exotic materials and advanced assembly processes, with an end result of streamlining the production costs and time for hypersonic aircraft; reducing months of assembly to weeks. Overall, this process greatly reduced the cost for producing hypersonic platforms. Even to such an extent that a Hellfire missile costs apx $100,000 but by utilizing our technologies, replacing it with a Mach 8-10 hypersonic missile of our physics/engineering and that missile would cost roughly $75,000 each delivered.
Materials used for these manufacturing processes are not disclosed, but overall, provides a foundation for extremely high stresses and thermodynamics, ideal for hypersonic platforms. This specific methodology and materials applications is many decades ahead of all known programs. Even to the extend of normalized space flight and re-entry, without concern of thermodynamic failure.
*Note, most entities that are experimenting with additive manufacturing for hypersonic aircraft, this makes it mainstream and standardized processes, which also applies for mass production.
What would normally be measured in years and perhaps a decade to go from drawing board to test flights, is reduced to singular months and ready for production within a year maximum.
Unified Turbine Based Combined Cycle (U-TBCC)
To date, the closest that NASA and industry have achieved for turbine based aircraft to fly at hypersonic velocities is by mounting a turbine into an aircraft and sharing the inlet with a scramjet or rocket based motor. Reaction Engines Sabre is not able to achieve hypersonic velocities and can only transition into a non air breathing rocket for beyond Mach 4.5
However, utilizing Unified Turbine Based Combine Cycle also known as U-TBCC, the two separate platforms are able to share a common inlet and the dual mode ramjet/scramjet is contained within the engine itself, which allows for a much smaller airframe footprint, thus engingeers are able to then design much higher performance aerial platforms for hypersonic flight, including the ability for constructing true single stage to orbit aircraft by utilizing a modification/version that allows for transition to outside atmosphere propulsion without any other propulsion platforms within the aircraft. By transitioning and developing aircraft to use Unified Turbine Based Combined Cycle, this propulsion system opens up new options to replace that airframe deficit for increased fuel capacity and/or payload.
Enhanced Dynamic Cavitation
Dramatically Increasing the efficiency of fuel air mixture for combustion processes at hypersonic velocities within scramjet propulsion platforms. The aspects of these processes are non disclosable.
Dynamic Scramjet Ignition Processes
For optimal scramjet ignition, a process known as Self Start is sought after, but in many cases if the platform becomes out of attitude, the scramjet will ignite. We have already solved this problem which as a result, a scramjet propulsion system can ignite at lower velocities, high velocities, at optimal attitude or not optimal attitude. It doesn't matter, it will ignite anyways at the proper point for maximum thrust capabilities at hypersonic velocities.
Hydrogen vs Kerosene Fuel Sources
Kerosene is an easy fuel to work with, and most western nations developing scramjet platforms use Kerosene for that fact. However, while kerosene has better thermal properties then Hydrogen, Hydrogen is a far superior fuel source in scramjet propulsion flight, do it having a much higher efficiency capability. Because of this aspect, in conjunction with our developments, it allows for a MUCH increased fuel to air mixture, combustion, thrust; and ability for higher speeds; instead of very low hypersonic velocities in the Mach 5-6 range. Instead, Mach 8-10 range, while we have begun developing hypersonic capabilities to exceed 15 in atmosphere within less then 5 years.
Conforming High Pressure Tank Technology for CNG and H2.
As most know in hypersonics, Hydrogen is a superior fuel source, but due to the storage abilities, can only be stored in cylinders thus much less fuel supply. Not anymore, we developed conforming high pressure storage technology for use in aerospace, automotive sectors, maritime, etc; which means any overall shape required for 8,000+ PSI CNG or Hydrogen. For hypersonic platforms, this means the ability to store a much larger volume of hydrogen vs cylinders.
As an example, X-43 flown by Nasa which flew at Mach 9.97. The fuel source was Hydrogen, which is extremely more volatile and combustible then kerosene (JP-7), via a cylinder in the main body. If it had used our technology, that entire section of the airframe would had been an 8,000 PSI H2 tank, which would had yielded 5-6 times the capacity. While the X-43 flew 11 seconds under power at Mach 9.97, at 6 times the fuel capacity would had yielded apx 66 seconds of fuel under power at Mach 9.97. If it had flew slower, around Mach 6, same principles applied would had yielded apx 500 seconds of fuel supply under power (slower speeds required less energy to maintain).
Enhanced Fuel Mixture During Shock Train Interaction
Normally, fuel injection is conducted at the correct insertion point within the shock train for maximum burn/combustion. Our methodologies differ, since almost half the fuel injection is conducted PRE shock train within the isolator, so at the point of isolator injection the fuel enhances the combustion process, which then requires less fuel injection to reach the same level of thrust capabilities.
Improved Bow Shock Interaction
Smoother interaction at hypersonic velocities and mitigating heat/stresses for beyond Mach 6 thermodynamics, which extraordinarily improves Type 3, 4, and 5 shock interaction.
6,000+ Fahrenheit Thermal Resistance
To date, the maximum thermal resistance was tested at AFRL in the spring of 2018, which resulted in a 3,200F thermal resistance for a short duration. This technology, allows for normalized hypersonic thermal resistance of 3,000-3,500F sustained, and up to 6,500F resistance for short endurance, ie 90 seconds or less. 10-20 minute resistance estimate approximately 4,500F +/- 200F.
*** This technology advancement also applies to Aerospike rocket engines, in which it is common for Aerospike's to exceed 4,500-5,000F temperatures, which results in the melting of the reversed bell housing. That melting no longer ocurrs, providing for stable combustion to ocurr for the entire flight envelope
Scramjet Propulsion Side Wall Cooling
With old technologies, side wall cooling is required for hypersonic flight and scramjet propulsion systems, otherwise the isolator and combustion regions of a scramjet would melt, even using advanced ablatives and ceramics, due to their inability to cope with very high temperatures. Using technology we have developed for very high thermodynamics and high stresses, side wall cooling is no longer required, thus removing that variable from the design process and focusing on improved ignition processes and increasing net thrust values.
Lower Threshold for Hypersonic Ignition
Active and adaptive flight dynamics, resulting in the ability for scramjet ignition at a much lower velocity, ie within ramjet envelope, between Mach 2-4, and seamless transition from supersonic to hypersonic flight, ie supersonic ramjet (scramjet). This active and dynamic aspect, has a wide variety of parameters for many flight dynamics, velocities, and altitudes; which means platforms no longer need to be engineered for specific altitude ranges or preset velocities, but those parameters can then be selected during launch configuration and are able to adapt actively in flight.
Dramatically Improved Maneuvering Capabilities at Hypersonic Velocities
Hypersonic vehicles, like their less technologically advanced brethren, use large actuator and the developers hope those controls surfaces do not disintegrate in flight. In reality, it is like rolling the dice, they may or may not survive, hence another reason why the attempt to keep velocities to Mach 6 or below. We have shrunken down control actuators while almost doubling torque and response capabilities specifically for hypersonic dynamics and extreme stresses involved, which makes it possible for maximum input authority for Mach 10 and beyond.
Paradigm Shift in Control Surface Methodologies, Increasing Control Authority (Internal Mechanical Applications)
To date, most control surfaces for hypersonic missile platforms still use fins, similar to lower speed conventional missiles, and some using ducted fins. This is mostly due to lack of comprehension of hypersonic velocities in their own favor. Instead, the body itself incorporates those control surfaces, greatly enhancing the airframe strength, opening up more space for hardware and fuel capacity; while simultaneously enhancing the platforms maneuvering capabilities.
A scramjet missile can then fly like conventional missile platforms, and not straight and level at high altitudes, losing velocity on it's decent trajectory to target. Another added benefit to this aspect, is the ability to extend range greatly, so if anyone elses hypersonic missile platform were developed for 400 mile range, falling out of the sky due to lack of glide capabilities; our platforms can easily reach 600+ miles, with minimal glide deceleration.
The Supermarine Spitfire, bred from the Schneider Trophy winning seaplane racers of the 30s, an incredibly elegant, agile and fast fighter, triumph of design and engineering. But oh so much more than that in the collective psyche of these islands, the Spit is forever associated with that moment when the history of the free world balanced on a knife edge, the Battle of Britain, and remains for many of us a supreme symbol of defiance against the odds in the face of overwhelming evil which had swallowed so much else but found the RAF more than they could chew...
This Spit was constructed late in the war, 1944, so long after that watershed air battle, although in the 1960s she would be taking to the air for part of the movie Battle of Britain. She's been the 'gate guard' at various RAF bases, including Leuchars, over the years and was eventually donated to the city of Glasgow (she had once been part of the City of Glasgow auxiliary RAF squadron in her history), refurbished at the National Museum of Flight at East Fortune and when the magnificent Kelvingrove Art Gallery & Museum re-opened after a huge redevelopment she was on display, hanging there amid the early 1900s architecture, rather delightfully right over the head of a stuffed giraffe on display with other animals below! There's something quite magical about turning into a wing of this huge, historic edifice and coming face to face with a real Spitfire just hanging there, the lines so elegant and aerodynamic she still looks fast even when hanging still...
A USAF F35 Lightning II performing during the Lightning demo at the 2025 Abbotsford International Airshow. It was an awesome demo, it was cut short however due to technical problems. A warning light came on and the pilot had to land. That said she put on a good show, didn't hold back, and she nearly broke the sound barrier.
R-2118 of fighter squadron 10 (Fliegerstaffel 10), stationed at Buochs airfield in Switzerland between 1965 and 2003.
This model in 1/32 scale is based on ILARAK Solutions' excellent design, whose instructions I bought.
After having built the model initially following the instructions, I have made quite some changes to the design to better represent the real aircraft with the identification R-2118:
- The first and main alteration was to move the wheels of the main landing gear outwards to represent the real Mirage's design. I also added landing gear bay covers to the struts.
- The nose landing gear now is much sleeker.
- Smoothed out the underside of the aircraft and added several details like vents. At the same time I was able to add representations of the two DEFA 30 mm cannons.
- Smoothed out the shaping around the cockpit and incorporated a new glass design.
- More detailed engine nozzle and vertical stabilizer.
- More realistic fragmentation of the control surfaces on the trailing edge of the wing.
- Slightly smoothed out the camo scheme.
- Added various under wing details like antennae and payload.
The landing gear is still fully functional, with the little drawback that with my chosen solution, the wheels are no longer able to rotate.
The under wing and fuselage details consist of (beginning at the wing tips):
- 2 x Radar warning antennae
- 2 x AIM-9B Sidewinder for self defense
- 2 x external fuel tank
- 2 x 4 JATO rockets for short take-off from partially destroyed runways
- Centerline reconnaissance pod
The Swiss Mirage III S and RS are a derivative of the French Mirage III, with "S" standing for Switzerland and "RS" for reconnaissance. Most of the Swiss Mirages were built in Switzerland under license. Changes over the French original included US avionics (thus the Sidewinder), reinforced structure for JATO take-offs and duck vanes added with combat value increase program.
There were 18 Mirages of the RS variant, numbered R-2101 to R-2118, with my model representing the last of the series. They featured four optical cameras in the nose section that could be equiped with different lenses and placed at different angles. Each camera had a film roll for 360 frames.
R-2118 carried the nickname "Mata Hari", the famous Dutch female spy of World War I. The name is painted on the left side of the cockpit section together with an owl.
Mirage III RS R-2118 still exists and is on display at the Air Force Center in Dübendorf near Zurich, Switzerland. My model represents the loadout of the real aircraft as exhibited.
To better display the details of the underside and the working landing gear, I built a display stand that shows the plane during take-off.
Spitfire stunt flying over East Preston
It arrived "out of the blue" and I thought it would only be over the village for a few seconds. How wrong I was. Anyway I grabbed the camera and poked it out the window to grab a couple of shots only to find he stayed around for several minutes. Time enough in fact to dash down the road to the beach and get some decent clear shots.
At the speed and altitude he was flying he only appeared in the gap between the roofs for a couple of seconds at the most on each pass.
IMG_6094
Via Collings Foundation: WINGS OF FREEDOM TOUR 2010 Schedule:
The B-17, B-24, and P-51 are on the 21st season of the Wings of Freedom Tour. Call 978-562-9182 to book your seat today!
The Wings of Freedom Tour brings historic aviation to your community! Tour through the authentically restored aircraft or take a flight aboard for the ultimate immersion in history!
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Via Collings Foundation: Aircraft Collection
For over twenty years The Collings Foundation has recovered and restored many of the true landmark aircraft that built world aviation history. Aircraft from the very roots of aviation up until the supersonic jets of modern day are represented in the collection which spans nearly 80 years of powered flight. Many of the aircraft are viewable to the public at airshows, events, and airports around the United States. For a schedule of these appearances, please visit our • schedules section. For groups interested in an appearance of these aircraft (with some exceptions) please visit our airshow & event booking section.
Early Aviation Collection
• 1909 Bleriot Type XI Stow, MA
• 1911 Wright Vin Fiz (Replica) Stow, MA (Static)
• 1917 Fokker DR-I Triplane (Replica) Stow, MA
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World War II Collection
• Boeing PT-17 Stearman Stow, MA
• Fiesler FI-156 Storch Stow, MA
• Grumman TBM Avenger Stow, MA
• Cessna UC-78 Bobcat Stow, MA
• North American A-36 Apache New Smyrna Beach , FL (Restoration)
• North American B-25J Mitchell"Tondelayo" New Smyrna Beach , FL
• Boeing B-17G Flying Fortress"Nine O Nine" New Smyrna Beach, FL
• Consolidated B-24J Liberator"Dragon and His Tail""All American""Witchcraft" New Smyrna Beach , FL
• North American TP-51C Mustang"Betty Jane" New Smyrna Beach , FL
• Messerschmitt Me 262 Schwalbe "White 1" New Smyrna Beach , FL
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Korean War Collection
• North American AT-6F Texan Stow, MA
• Douglas A-26 Invader"My Mary Lou" Uvalde, TX (Restoration)
• Vought F4U-5NL Corsair New Smyrna Beach, FL
• Lockheed T-33 Shooting Star Stow, MA (Static Only)
• Lockheed T-33 Shooting Star Houston, TX (Restoration)
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Vietnam War Collection
• Bell UH-1E Huey Houston, TX
• Grumman S-2F Tracker Houston, TX
• McDonnell TA-4J Skyhawk Houston, TX
• McDonnell Douglas F-4D Phantom Houston, TX
This sopwith camel fighter plane, flown by one of Snoopy's alter egos, was designed and built by airplane hobbyist, Jack Williams of Rice Lake, Wisconsin in 1978. On May 12, 2001, he donated it to the Snoopy Gallery and Gift Shop in Memory of Charles Schulz.
Snoopy first appeared as the World War I Flying Ace in October, 1965. Since then the adventures of the fictional dog chasing the famous German ace pilot, Baron Von Richthoven, have filled comic pages and television screens.
Snoopy's Gallery & Gift Shop, located next to the Redwood Empire Ice Arena at 1665 West Steele Lane in Santa Rosa, features 2,400 square feet of a wide range of Peanuts products.
Off-Airport - Valdosta
Pendleton Park
Valdosta, GA
North American F-86L-50-NA Sabre (NA-190) c/n 190-782, 52-10057 / FU-057 / MY, United States Air Force
Pictured here where she stood for fifty years, looking a little faded, but still presentable. On April 24, 2012, this old Sabre was removed from her plinths, and transported back to nearby Moody AFB to be prepared for a new display there. Newly repainted, the aircraft was dedicated in a ceremony on April 27, 2013, at the "George W Bush Airpark" at Moody AFB.
Originally built as an F-86D-50-NA, modified as an F-86L under Project Follow-On, with modifications notably including the ability to use the SAGE datalink network for ground controlled interception.
Its active phase commenced in 1917, and ceased in 1959 when RAF Fighter Command left the aerodrome. The airfield at Kenley now hosts 615 Volunteer Gliding Squadron (VGS), a Royal Air Force gliding squadron of the Air Cadet Organisation.
During World War II RAF Kenley was one of the three main fighter stations, which was, together with Croydon and Biggin Hill, responsible for the air defence of London. It was during the crucial days of the Battle of Britain that all three RAF stations came into their own, fighting off the overwhelming might of the German Luftwaffe.
RAF Kenley suffered its worst damage in an attack on 18 August 1940. September 15 is considered by many to be the climax of the Battle of Britain, but 18 August is often cited as the costliest or hardest - the British lost 68 aircraft and the Germans lost 69. At Kenley, all ten hangars and twelve aircraft, including ten Hurricanes, were destroyed and the runways badly cratered. The Sector Operations Room had to be moved to an emergency location away from the airfield.
The pilots
Many famous pilots are connected or served at Kenley, including the famous South Africans 'Sailor' Malan, Group Captain P.H. 'Dutch' Hugo and the British ace JE "Johnnie" Johnson, later Air Vice-Marshal, who took over the Canadian wing at Kenley in 1943. The aerodrome was used as a location in the following films: Angels One Five (1952) and Reach for the Sky (1956), the latter about Douglas Bader who was posted to RAF Kenley in 1930 No. 23 Squadron RAF shortly before his accident in 1931
The present
Although few of the remaining buildings survive and the control tower was demolished after a fire in 1978 along with the hangars, Kenley is thought to be the best preserved of all WWII RAF fighter stations, with the runway still in its original configuration. English Heritage (in 2000) identified Kenley as "The most complete fighter airfield associated with the Battle of Britain to have survived". The respective councils of Croydon and Tandridge have designated the airfield site as a Conservation Area (2006)
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