View allAll Photos Tagged Iteration
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The first iteration of the Banana Republic "tagless" tee included a huge RFID tag inside the shirt at the waistline.
Now, it's a regular tag at the waistline which is actually MORE itchy than a collar tag. It scratches your waist... as by nature, it's tucked inside your pants. Pretty hilarious. It's also, very tough to remove without putting a hole in the shirt.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
Another iteration of my M83 image (http://www.flickr.com/photos/stars/2565181428/). This time i concentrated on the red channel, because i realized that most of the noise and vignetting of the image was there. All processed with Pixinsight. Comments are welcome =)
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Reproceso de mi imagen de M83. (http://www.flickr.com/photos/stars/2565181428/) Esta vez, separé cada uno de los colores y trabajé especialmente el canal rojo, ya que me dí cuenta que contenía casi todo el ruido y gran parte del viñeteo causado por la contaminación lumínica. Todo procesado con Pixinsight. Se agradecen los comentarios =)
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
Document name:CenterOff3 800x800e.FWrk
Fractal type:mandelbrot
Plot size (w,h):800,800
Maximum iterations:65535
Center Point (real, imaginary):-0.495860660910837,0.524373533386701 i
Plot Width (real):4.69E-13
Color scheme name:Lipstick
Color scheme last modified:2008-08-27 10:31:08 -0700
Plot uses DE:Yes
Plot uses fractaional iterations:Yes
Plotted with symmetry:Yes
Plotted with boundary following:Yes
Plotted with multiple processors:Yes
Total plot time:0.000 seconds
Total iterations:1817183654
Iterations/second:2147483647
Pixels skipped:0
Iterations skipped:0
Percent of pixels calculated:100
Percent of iterations calculated:100
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
Once I got the basic design of the button down (let's call it a sort of square top hat) I spent a bunch of time iterating - making slightly different versions, jamming them in my pocket, and trying to get them to fault.
While I was doing this lilia was ninja chopping the code. We still need to develop how we process the signals. Signal processing, ah. What does a button press look like? How long should it send a signal for? How long should it wait before sending another one?
BlueEdge - Mach 8-10 Hypersonic Commercial Aircraft, 220 Passenger Hypersonic Commercial Plane - Iteration 3
Seating: 220 | Crew 2+4
Length: 195ft | Span: 93ft
Engines: 4 U-TBCC (Unified Turbine Based Combined Cycle) +1 Aerospike for sustained 2G acceleration to Mach 10.
Fuel: H2 (Compressed Hydrogen)
Cruising Altitude: 100,000-125,000ft
Airframe: 75% Proprietary Composites
Operating Costs, Similar to a 737. $7,000-$15,000hr, including averaged maintenence costs
Iteration 3 (Full release of IT3, Monday January 14, 2019)
IO Aircraft www.ioaircraft.com
Drew Blair www.linkedin.com/in/drew-b-25485312/
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hypersonic plane, hypersonic aircraft, hypersonic commercial plane, hypersonic commercial aircraft, hypersonic airline, 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
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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 department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
Zoom into the "Mandelbrot set" for the map zn+1=Mi(zn)2, where Mi(z) are three Möbius transforms cyclically applied after each other. The transforms are -1/z, (-0.43-i)/((3-.1i)z - i), (wz-i)/(iz+.3+.1*i) where w is used as the control parameter varying across the images. z starts from zero, and the location after 300 iterations derermines the color (angle determines hue, magnitude value). The colored blobs represent areas where zero is attracted to the same limit cycle.
"First iteration" area represent the initial knowledge we gave Gabi;
"Second iteration" is the upate to Gabi's knowledge;
The long tail is the problem we're now facing: how can we manage an Artificial Intelliogence with such a parcellization of know-how?
Leeander was so kind to cite this graph in his World Business Forum talk.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The 2013 iteration of InformalScience.org sets a new standard for sharing informal science education projects, evaluation, and research resources. Learn more about the website at: ideum.com/media-web-design/premier-informal-science-educa...
museumPASSmusees 2024 - Wiels - Jana Euler - Alexis Blake
Jana Euler?s exhibition Oilopa, a contraction of the terms Oil (painting) and Europa, unfolds into a semi-utopian land, reversing the ascendant flows of financial figures while extrapolating on cycles of surplus and vacuity.
Originally conceived as a performance, Crack Nerve Boogie Swerve embraces concepts such as transparency, resistance, resonance and disruption?breaking free from norms, liberating oneself from the constraints of oppression and stretching the boundaries of art institutions. At WIELS, Alexis Blake (b. 1981, US/NL) expands the scope of a live work into a performative exhibition that encapsulates its past iterations while slowly transforming the present one.
WIELS est l'une des plus d?importantes institutions d'art contemporain en Europe. Sans constituer de collection permanente, WIELS se consacre a la presentation et a la production d?expositions temporaires d?artistes nationaux et internationaux, aussi bien des talents emergents que des valeurs etablies.
( Le pass musees, comment ca marche ?
1 pass pour 244 musees
Tant de choses a vivre avec le pass musees
Le pass musees est l?abonnement le plus genereux aux musees belges. Cela signifie :
*Acces a tous les musees participants de notre pays, pendant une annee entiere. Quand vous le voulez et aussi souvent que vous le souhaitez.
*Visiter les expositions temporaires gratuitement ou avec une jolie reduction.
*Beneficier d?Avantages extra comme des billets de train a moitie prix, des reductions dans les boutiques des musees et de nombreux autres cadeaux reserves exclusivement aux detenteurs de pass musees.
*Recevoir et sauvegarder les meilleurs conseils en matiere de musees : tous les quinze jours, recevez dans votre boite mail des informations sur les expositions a ne pas manquer et les plus belles decouvertes a faire dans les musees. Vous pouvez sauvegarder vos expositions preferees dans l?app pass musees en prevision de votre prochaine visite.
The first iteration of the infamous Initial D drift game. Imagine an arcade racer with a build in career mode. It keeps track of you career with your own ID-card. The printer works great, screen looks awesome and the overall cabinet is in a great state.
mju 820 - September 2010
Quite noisy... the mju doesn't work so well in low light conditions. I've added some vigneting to avoid distracting from the main subjects.
The last iteration of the famed Seville name, before giving way to a "STS" only line-up and disappearing completely a few years later. Too bad the owner chose to fit some tacky aftermarket chromed wheels! You can tell it's a pre-2002 model because it still sports the classic Cadillac emblem: starting with the 2002 model year and the introduction of the CTS, all models switched to the Arts and Science version of the logo. Still a big, brash and proud American sedan!
Chippewa 350 - 14 Passenger Medium Lift VTOL Fixed Wing Aircraft - Iteration 1
www.ioaircraft.com/vtol/Chippewa350.php
Passengers: 14 Commercial / 21 Military
Total Length: 45'
Total Span: 38' 5"
Power: 2 X U-GTG Turbine (H2/Kero) / 88 X 2.5KW Fuel Cells
Motors: 4 Time Super Magnetic Graphene Based
Range: 1,000+ NM Kero or H2 Exclusively / 2,000 NM, Both Simultaneously
Performance: 350 KT Cruise
Safety: Aircraft also equipped with a BRS (Ballistic Recovery System)
This has been on the drawing board Per se (years of other developments into a new aircraft design) for a long time, it's not a priority, I was bored so I finalized iteration 1.
All technologies developed. Even the wings, they are not hinged control surfaces but wing warping control surfaces. H2/Kero Hybdrid and can switch between either
Rotors are HIGH thrust supersonic with shock elimination. Motors are all graphene based (double S/HP and NO HEAT), Engines U-GTG. At forward flight, rotors (not props) then cycle down the rpm as needed but cruises well above 300kts. Flight dynamics are high performance, unlike the V-22 Osprey. Turbines are mainly for 350kt cruise.
Overall Estimates are accurate. This is first images on the net. There are not even landing pages for it or on other platforms (yet)
bae, sikorsky, bell, boeing, lockheed martin, raytheon, northrop grumman, airbus, afrl, onr, arl, usarmy, vtol, evtol, hydrogen, innovation, nasa, aerospace, engineering, aeronautics, science, aircraft, urban air mobility, advanced air mobility, electric propulsion, rotocraft, helicopter, drone, transportion, v280, V22, Osprey, USCG, USNavy, aam, epav, flying car, hevstol, orlandoflorida, uber, electric vtol, air taxi, vertical take off and landing, hydrogen aviation, hydrogen aircraft, hydrogen vtol, hydrogen commercial aircraft, chippewa, darpa, defense advanced research agency, boeing phantom works, lockheed skunk works
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
A U.S. Marine with Marine Heavy Helicopter Squadron 466 ‘Wolfpack’ unloads equipment from a CH-53E Super Stallion on the runway at U-Tapao International Airport, Kingdom of Thailand, Feb. 10, 2018. HMH-466 ‘Wolfpack’ arrive to the Kingdom of Thailand to participate in the 37th iteration of Cobra Gold as part of the U.S. Marine Corps Aviation Combat Element. The Super Stallion is assigned to HMH-466, Marine Aircraft Group 16, 3rd Marine Aircraft Wing, currently forward deployed under the unit deployment program with MAG-36, 1st MAW, based out of Okinawa, Japan. Exercise Cobra Gold 2018 is an annual exercise conducted in the Kingdom of Thailand held from Feb. 13-23 with seven full participating nations. (U.S. Marine Corps photo by Cpl. Andy Martinez)
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
Chippewa 350 - 14 Passenger Medium Lift VTOL Fixed Wing Aircraft - Iteration 1
www.ioaircraft.com/vtol/Chippewa350.php
Passengers: 14 Commercial / 21 Military
Total Length: 45'
Total Span: 38' 5"
Power: 2 X U-GTG Turbine (H2/Kero) / 88 X 2.5KW Fuel Cells
Motors: 4 Time Super Magnetic Graphene Based
Range: 1,000+ NM Kero or H2 Exclusively / 2,000 NM, Both Simultaneously
Performance: 350 KT Cruise
Safety: Aircraft also equipped with a BRS (Ballistic Recovery System)
This has been on the drawing board Per se (years of other developments into a new aircraft design) for a long time, it's not a priority, I was bored so I finalized iteration 1.
All technologies developed. Even the wings, they are not hinged control surfaces but wing warping control surfaces. H2/Kero Hybdrid and can switch between either
Rotors are HIGH thrust supersonic with shock elimination. Motors are all graphene based (double S/HP and NO HEAT), Engines U-GTG. At forward flight, rotors (not props) then cycle down the rpm as needed but cruises well above 300kts. Flight dynamics are high performance, unlike the V-22 Osprey. Turbines are mainly for 350kt cruise.
Overall Estimates are accurate. This is first images on the net. There are not even landing pages for it or on other platforms (yet)
bae, sikorsky, bell, boeing, lockheed martin, raytheon, northrop grumman, airbus, afrl, onr, arl, usarmy, vtol, evtol, hydrogen, innovation, nasa, aerospace, engineering, aeronautics, science, aircraft, urban air mobility, advanced air mobility, electric propulsion, rotocraft, helicopter, drone, transportion, v280, V22, Osprey, USCG, USNavy, aam, epav, flying car, hevstol, orlandoflorida, uber, electric vtol, air taxi, vertical take off and landing, hydrogen aviation, hydrogen aircraft, hydrogen vtol, hydrogen commercial aircraft, chippewa, darpa, defense advanced research agency, boeing phantom works, lockheed skunk works
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
Recursive Iterations,
Words that delve into spirals
of Chaos and present us with
our world in ordered randomness.
Give the computer numbers,
Wait patiently,
And emergent patterns
imitate familiar objects in life.
As if a genie rubbed a lamp,
The mouse presses awe into motion, and I get to share my awe and excitement.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.
The department has been building up a library of design related reference books over the last few years. Pupils are encouraged to make use of these books on a regular basis. The photographs here demonstrate the tremendous wealth of content contained therein.
The sequence has been shot in such a way that the cover of the book is shown first and a few sample pages are included to give the student an idea of the content the book contains. Pupils may then approach staff and request a short term loan.