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Showing posts with label Concept. Show all posts
Showing posts with label Concept. Show all posts

Saturday, October 24, 2015

Lockheed SR-75 Aurora

Here are some images plus a composite of Testor's 1/72 scale Lockheed? SR-75 Aurora. The following is taken from the Aurora Aircraft Page. "In the late 1980s and early 1990s it was believed that a top-secret reconnaissance aircraft, capable of flying at speeds beyond Mach 6, was developed to replace the SR-71 Blackbird. The alleged project was detailed in mainstream media including the New York Times, the Wall Street Journal, Jane's Defence Weekly, and Aviation Week & Space Technology.

The name Aurora was included in a Pentagon budget request in 1985, perhaps inadvertently, underneath reconnaissance programs of the SR-71 and U-2. The Aurora has been attributed to scores of unidentified aircraft reports around the world, including a 1989 sighting from an oil platform in the North Sea, a series of mysterious sonic booms over Southern California in 1991-92, and photographs of unusual "donuts-on-a-rope" contrails. 


From Wikipedia"

Aurora was a rumored mid-1980s American reconnaissance aircraft. There is no substantial evidence that it was ever built or flown and it has been termed a myth.
The U.S. government has consistently denied such an aircraft was ever built. Aviation and space reference site Aerospaceweb.org concluded "The evidence supporting the Aurora is circumstantial or pure conjecture, there is little reason to contradict the government's position."
Others come to different conclusions. In 2006, veteran black project watcher and aviation writer Bill Sweetman said, "Does Aurora exist? Years of pursuit have led me to believe that, yes, Aurora is most likely in active development, spurred on by recent advances that have allowed technology to catch up with the ambition that launched the program a generation ago."
 The Aurora legend started in March 1990, when Aviation Week & Space Technology magazine broke the news that the term "Aurora" had been inadvertently included in the 1985 U.S. budget, as an allocation of $455 million for "black aircraft production" in FY 1987. According to Aviation Week, Project Aurora referred to a group of exotic aircraft, and not to one particular airframe. Funding of the project allegedly reached $2.3 billion in fiscal 1987, according to a 1986 procurement document obtained by Aviation Week. In the 1994 book Skunk Works, Ben Rich, the former head of Lockheed's Skunk Works division, wrote that the Aurora was the budgetary code name for the stealth bomber fly-off that resulted in the B-2 Spirit.By the late 1980s, many aerospace industry observers believed that the U.S. had the technological capability to build a Mach-5 replacement for the aging Lockheed SR-71 Blackbird. Detailed examinations of the U.S. defense budget claimed to have found money missing or channeled into black projects. By the mid-1990s, reports surfaced of sightings of unidentified aircraft flying over California and the United Kingdom involving odd-shaped contrails, sonic booms and related phenomena that suggested the US had developed such an aircraft. Nothing ever linked any of these observations to any program or aircraft type, but the name Aurora was often tagged on these as a way of explaining the observations.


In late August 1989, while working as an engineer on the jack-up barge GSF Galveston Key in the North Sea, Chris Gibson and another witness saw an unfamiliar isosceles triangle-shaped delta aircraft, apparently refueling from a Boeing KC-135 Stratotanker and accompanied by a pair of F-111 fighter-bombers. Gibson and his friend watched the aircraft for several minutes, until they went out of sight. He subsequently drew a sketch of the formation.
Gibson, who had been in the Royal Observer Corps' trophy-winning international aircraft recognition team since 1980, was unable to identify the aircraft. He dismissed suggestions that the aircraft was an F-117, Mirage IV or fully swept wing F-111. When the sighting was made public in 1992, the British Defence Secretary Tom King was told, "There is no knowledge in the MoD of a 'black' programme of this nature, although it would not surprise the relevant desk officers in the Air Staff and Defence Intelligence Staff if it did exist."
A crash at RAF Boscombe Down in Wiltshire on 26 September 1994 appeared closely linked to "black" missions, according to a report in AirForces Monthly. Further investigation was hampered by aircraft from the USAF flooding into the base. The crash site was protected from view by firetrucks and tarpaulins and the base was closed to all flights soon after.

A series of unusual sonic booms was detected in Southern California, beginning in mid- to late-1991 and recorded by United States Geological Survey sensors across Southern California used to pinpoint earthquake epicenters. The sonic booms were characteristic of a smaller vehicle, rather than the 37-meter long Space Shuttle orbiter. Furthermore, neither the Shuttle nor NASA's single SR-71B was operating on the days the booms had been registered. In the article, "In Plane Sight?" which appeared in the Washington City Paper on 3 July 1992 (pp. 12–13), one of the seismologists, Jim Mori, noted: "We can't tell anything about the vehicle. They seem stronger than other sonic booms that we record once in a while. They've all come on Thursday mornings about the same time, between 4 and 7." Former NASA sonic boom expert Dom Maglieri studied the 15-year-old sonic boom data from the California Institute of Technology and has deemed that the data showed "something at 90,000 ft (c. 27.4 km), Mach 4 to Mach 5.2". He also said the booms did not look like those from aircraft that had traveled through the atmosphere many miles away at Los Angeles International Airport, rather, they appeared to be booms from a high-altitude aircraft directly above the ground moving at high speeds. The boom signatures of the two different aircraft patterns are wildly different. There was nothing particular to tie these events to any aircraft, but they served to grow the Aurora legend.
On 23 March 1992, near Amarillo, Texas, Steven Douglass photographed the "donuts on a rope" contrail and linked this sighting to distinctive sounds. He described the engine noise as: "strange, loud pulsating roar... unique... a deep pulsating rumble that vibrated the house and made the windows shake... similar to rocket engine noise, but deeper, with evenly timed pulses." In addition to providing the first photographs of the distinctive contrail previously reported by many, the significance of this sighting was enhanced by Douglass' reports of intercepts of radio transmissions: "Air-to-air communications... were between an AWACS aircraft with the call sign "Dragnet 51" from Tinker AFB, Oklahoma, and two unknown aircraft using the call signs "Darkstar November" and "Darkstar Mike". Messages consisted of phonetically transmitted alphanumerics. It is not known whether this radio traffic had any association with the "pulser" that had just flown over Amarillo." ("Darkstar" is also a call sign of AWACS aircraft from a different squadron at Tinker AFB) A month later, radio enthusiasts in California monitoring Edwards AFB Radar (callsign "Joshua Control") heard early morning radio transmissions between Joshua and a high flying aircraft using the callsign "Gaspipe". "You're at 67,000 feet, 81 miles out" was heard, followed by "70 miles out now, 36,000 ft, above glideslope." As in the past, nothing linked these observations to any particular aircraft or program, but the attribution to the Aurora helped expand the legend.
In February 1994 former resident of Rachel, Nevada, and Area 51 enthusiast, Chuck Clark claimed to have filmed the Aurora taking off from the Groom Lake facility. In the David Darlington book Area 51: The Dreamland Chronicles, he said:
I even saw the Aurora take off one night - or an aircraft that matched the Aurora's reputed configuration, a sharp delta with twin tails about a hundred and thirty feet long. It taxied out of a lighted hangar at two-thirty A.M. and used a lot of runway to take off. It had one red light on top, but the minute the wheels left the runway, the light went off and that was the last I saw of it. I didn't hear it because the wind was blowing from behind me toward the base." I asked when this had taken place. "February 1994. Obviously they didn't think anybody was out there. It was thirty below zero - probably ninety below with the wind chill factor. I had hiked into White Sides from a different, harder way than usual, and stayed there two or three days among the rocks, under a camouflage tarp with six layers of clothes on. I had an insulated face mask and two sleeping bags, so I didn't present a heat signature. I videotaped the aircraft through a telescope with a five-hundred-millimeter f4 lens coupled via a C-ring to a high-eight digital video camera with five hundred and twenty scan lines of resolution, which is better than TV." The author then asked "Where's the tape?" Locked away. That's a legitimate spyplane; my purpose is not to give away legitimate national defense. When they get ready to unveil it, I'll probably release the tape.

Although his claims have been controversial, Bob Lazar has stated that, during his employment at the mysterious S-4 facility in Nevada, he briefly witnessed an Aurora flight while aboard a bus near Groom Lake. He claimed that there was a "tremendous roar" which sounded almost as though "the sky was tearing". Although Lazar only saw the aircraft for a moment through the front of the bus, he described it as being "very large" and having "two huge, square exhausts with vanes in them". Lazar claims that his supervisor confirmed to him that the aircraft was indeed an "Aurora", a "high altitude research plane". He was also told that the aircraft was powered by "liquid methane".
By 1996, reports associated with the Aurora name dropped off in frequency, suggesting to people who believed that the aircraft existed that it had only ever been a prototype or that it had had a short service life.
In 2000, Aberdeen Press and Journal writer Nic Outterside wrote a piece on US stealth technology in Scotland. Citing confidential 'sources', he alleged RAF/USAF Machrihanish in Kintyre, Argyll to be a base for Aurora aircraft. Machrihanish's almost 2-mile (3.2 km)-long long runway makes it suitable for high-altitude and experimental aircraft with the fenced-off coastal approach making it ideal for takeoffs and landings to be made well away from eyes or cameras of press and public. 'Oceanic Air Traffic Control at Prestwick' Outterside says, 'also tracked fast-moving radar blips. It was claimed by staff that a "hypersonic jet was the only rational conclusion" for the readings.'
In 2006, aviation writer Bill Sweetman put together 20 years of examining budget "holes", unexplained sonic booms, as well as the Gibson sighting and concluded:
"This evidence helps establish the program's initial existence. My investigations continue to turn up evidence that suggests current activity. For example, having spent years sifting through military budgets, tracking untraceable dollars and code names, I learned how to sort out where money was going. This year, when I looked at the Air Force operations budget in detail, I found a $9-billion black hole that seems a perfect fit for a project like Aurora."
On 1 December 2014, loud repetitive bangs were heard in Bedfordshire, Glasgow, North Devon, Leicestershire, and West Sussex in the UK. The repetitive banging sound lasted for 20 to 30 minutes and was recorded by one resident on a cell phone. At around the same time, a loud boom was reported by a number of people in the upstate New York areas of Buffalo, Cheektowaga, and Clarence. Dr Bhupendra Khandelwa (University of Sheffield, UK) stated that he believed the loud, repetitive bangs sounded like an experimental jet engine called a pulse detonation engine (PDE). Sonic booms caused by meteors and military planes were ruled out, as were the sounds of fireworks and thunderstorms. Media speculation concluded that the noise recorded by locals in the UK could have been caused by the PDE engine of an Aurora aircraft.
 

Tuesday, July 8, 2014

Mig 37-E Ferret

Here are some more images plus a composite of Italeri's 1/48 scale Mikoyan Mig 37-E Ferret. This is a fictional aircraft designed by Italeri/Testor's as a follow up to their F-19 Stealth fighter. The MiG-37 is a stealth fighter designed using advances in technology from the Soviet Union's space and aviation programs as a reaction to the American F-19 stealth project.

F-19 A Specter

Here are some more images of Monogram's 1/48 scale Lockheed? F-19A Stealth Reconnaissance/Fighter "Specter". This is one of the speculative designs that model kit companies were coming out with on what they thought the new stealth fighter may look like back in the 1980s. Which of coarse turned out to be the F-117 fighter bomber and as you can see Monogram was way off. The design of this model actually came from concept drawings from the Loral corporation a defense contractor founded in 1948. The reason for the F-19 moniker is that the number 19 has never been officially assigned to any aircraft which of coarse leads one to believe that the F-19 is a highly classified and secretive aircraft, very strange. The F-18 is the McDonnell Douglas (now Boeing) Hornet/Super Hornet and the F-20 is the Northrop Tigershark but no F-19, Why? It is indeed a Specter.

Friday, August 24, 2012

Friday, February 24, 2012

Monday, February 6, 2012

Orion Nuclear Starship




Here are some images of my scratch built Orion Nuclear Starship, based off off earlier drawings of the concept.

From Wikipedia"

Project Orion was a study of a spacecraft intended to be directly propelled by a series of explosions of atomic bombs behind the craft (Nuclear pulse propulsion). Early versions of this vehicle were proposed to have taken off from the ground with significant associated nuclear fallout; later versions were presented for use only in space.

A 1955 Los Alamos Laboratory document states (without offering references) that general proposals were first made by Stanislaw Ulam in 1946, and that preliminary calculations were made by F. Reines and Ulam in a Los Alamos memorandum dated 1947. The actual project, initiated in 1958, was led by Ted Taylor at General Atomics and physicist Freeman Dyson, who at Taylor's request took a year away from the Institute for Advanced Study in Princeton to work on the project.

By using energetic nuclear power, the Orion concept offered high thrust and high specific impulse, or propellant efficiency, at the same time. As a qualitative comparison, traditional chemical rockets—such as the Saturn V that took the Apollo program to the Moon—produce high thrust with low specific impulse, whereas electric ion engines produce a small amount of thrust very efficiently. Orion would have offered performance greater than the most advanced conventional or nuclear rocket engines then under consideration. Supporters of Project Orion felt that it had potential for cheap interplanetary travel, but it lost political approval over concerns with fallout from its propulsion. The Partial Test Ban Treaty of 1963 is generally acknowledged to have ended the project.

The Orion nuclear pulse drive combines a very high exhaust velocity, from 20 to 30 km/s, with meganewtons of thrust. Many spacecraft propulsion drives can achieve one of these or the other, but nuclear pulse rockets are the only proposed technology that could potentially deliver both (see spacecraft propulsion for more speculative systems). Specific impulse measures how much thrust can be derived from a given mass of fuel, and is the standard figure of merit for rocketry.

Since weight is no limitation, an Orion craft can be extremely robust. An unmanned craft could tolerate very large accelerations, perhaps 100 g. A human-crewed Orion, however, must use some sort of damping system behind the pusher plate to smooth the instantaneous acceleration to a level that humans can comfortably withstand – typically about 2 to 4 g.

The high performance depends on the high exhaust velocity, in order to maximize the rocket's force for a given mass of propellant. The velocity of the plasma debris is proportional to the square root of the change in the temperature (Tc) of the nuclear fireball. Since fireballs routinely achieve ten million degrees Celsius or more in less than a millisecond, they create very high velocities. However, a practical design must also limit the destructive radius of the fireball. The diameter of the nuclear fireball is proportional to the square root of the bomb's explosive yield.

The shape of the bomb's reaction mass is critical to efficiency. The original project designed bombs with a reaction mass made of tungsten. The bomb's geometry and materials focused the X-rays and plasma from the core of nuclear explosive to hit the reaction mass. In effect each bomb would be a nuclear shaped charge.

A bomb with a cylinder of reaction mass expands into a flat, disk-shaped wave of plasma when it explodes. A bomb with a disk-shaped reaction mass expands into a far more efficient cigar-shaped wave of plasma debris. The cigar shape focuses much of the plasma to impinge onto the pusher-plate.

where C0 is the collimation factor (what fraction of the explosion plasma debris will actually hit the impulse absorber plate when a pulse unit explodes), Ve is the nuclear pulse unit plasma debris velocity, and gn is the standard acceleration of gravity (9.81 m/s2; this factor is not necessary if Isp is measured in N·s/kg or m/s). A collimation factor of nearly 0.5 can be achieved by matching the diameter of the pusher plate to the diameter of the nuclear fireball created by the explosion of a nuclear pulse unit.

The smaller the bomb, the smaller each impulse will be, so the higher the rate of impulses and more than will be needed to achieve orbit. Smaller impulses also mean less g shock on the pusher plate and less need for damping to smooth out the acceleration.

The optimal Orion drive bomblet yield (for the human crewed 4,000 ton reference design) was calculated to be in the region of 0.15 KT, with approx 800 bombs needed to orbit and a bomb rate of approx 1 per second.

Friday, February 3, 2012

Daedalus





Here are some images of my scratch build model of the Daedalus Spacecraft.

From Wikipedia"

Project Daedalus was a study conducted between 1973 and 1978 by the British Interplanetary Society to design a plausible unmanned interstellar spacecraft. Intended mainly as a scientific probe, the design criteria specified that the spacecraft had to use current or near-future technology and had to be able to reach its destination within a human lifetime. Alan Bond led a team of scientists and engineers who proposed using a fusion rocket to reach Barnard's Star, only 5.9 light years away. The trip was estimated to take 50 years, but the design was required to be flexible enough that it could be sent to any of a number of other target stars.

Daedalus would be constructed in Earth orbit and have an initial mass of 54,000 tonnes, including 50,000 tonnes of fuel and 500 tonnes of scientific payload. Daedalus was to be a two-stage spacecraft. The first stage would operate for two years, taking the spacecraft to 7.1% of light speed (0.071 c), and then after it was jettisoned the second stage would fire for 1.8 years, bringing the spacecraft up to about 12% of light speed (0.12 c) before being shut down for a 46-year cruise period. Due to the extreme temperature range of operation required (from near absolute zero to 1,600 K) the engine bells and support structure would be made of molybdenum TZM alloy, which retains strength even at cryogenic temperatures. A major stimulus for the project was Friedwardt Winterberg's inertial confinement fusion drive concept for which he received the Hermann Oberth gold medal award.

This velocity is well beyond the capabilities of chemical rockets, or even the type of nuclear pulse propulsion studied during Project Orion. Instead, Daedalus would be propelled by a fusion rocket using pellets of deuterium/helium-3 mix that would be ignited in the reaction chamber by inertial confinement using electron beams. The electron beam system would be powered by a set of induction coils tapping energy from the plasma exhaust stream. 250 pellets would be detonated per second, and the resulting plasma would be directed by a magnetic nozzle. The computed burn-up fraction for the fusion fuels was 0.175 and 0.133 for the First & Second stages, producing exhaust velocities of 10,600 km/s and 9,210 km/s, respectively. Due to the scarcity of helium-3 it was to be mined from the atmosphere of Jupiter via large hot-air balloon supported robotic factories over a 20 year period.

The second stage would have two 5-meter optical telescopes and two 20-meter radio telescopes. About 25 years after launch these telescopes would begin examining the area around Barnard's Star to learn more about any accompanying planets. This information would be sent back to Earth, using the 40-meter diameter second stage engine bell as a communications dish, and targets of interest would be selected. Since the spacecraft would not decelerate upon reaching Barnard's Star, Daedalus would carry 18 autonomous sub-probes that would be launched between 7.2 and 1.8 years before the main craft entered the target system. These sub-probes would be propelled by nuclear-powered ion drives and carry cameras, spectrometers, and other sensory equipment. They would fly past their targets, still travelling at 12% of the speed of light, and transmit their findings back to the Daedalus second stage mothership for relay back to Earth.

The ship's payload bay containing its sub-probes, telescopes, and other equipment would be protected from the interstellar medium during transit by a beryllium disk up to 7 mm thick and weighing up to 50 tonnes. This erosion shield would be made from beryllium due to its lightness and high latent heat of vaporisation. Larger obstacles that might be encountered while passing through the target system would be dispersed by an artificially generated cloud of particles, ejected by support vehicles called dust bugs, some 200 km ahead of the vehicle. The spacecraft would carry a number of robot "wardens" capable of autonomously repairing damage or malfunctions.


Tuesday, January 10, 2012

Bussard Ramjet





Here are some images of my scratch built concept engine/ship of the Bussard Ramjet.

From Wikipedia"

The Bussard ramjet is a theoretical method of spacecraft propulsion proposed in 1960 by the physicist Robert W. Bussard, popularized by Larry Niven in his Known Space series of books, and referred to by Carl Sagan in the television series and book Cosmos.

Bussard proposed a ramjet variant of a fusion rocket capable of reasonable interstellar spaceflight, using enormous electromagnetic fields (ranging from kilometers to many thousands of kilometers in diameter) as a ram scoop to collect and compress hydrogen from the interstellar medium. High speeds force the reactive mass into a progressively constricted magnetic field, compressing it until thermonuclear fusion occurs. The magnetic field then directs the energy as rocket exhaust opposite to the intended direction of travel, thereby accelerating the vessel.

A major problem with using rocket propulsion to reach the velocities required for interstellar flight is the enormous amounts of fuel required. Since that fuel must itself be accelerated, this results in an approximately exponential increase in mass as a function of velocity change at non-relativistic speeds, asymptotically tending to infinity as it approaches the speed of light. In principle, the Bussard ramjet avoids this problem by not carrying fuel with it. An ideal ramjet design could in principle accelerate indefinitely until its mechanism failed. Ignoring drag, a ship driven by such an engine could theoretically accelerate arbitrarily close to the speed of light, and would be a very effective interstellar spacecraft. In practice, since the force of drag produced by collecting the interstellar medium increases approximately as its speed squared at non-relativistic speeds and asymptotically tends to infinity as it approaches the speed of light (taking all measurements from the ship's perspective), any such ramjet would have a limiting speed where the drag equals thrust. To produce positive thrust, the fusion reactor must be capable of producing fusion while still giving the incident ions a net rearward acceleration (relative to the ship).

Tuesday, May 3, 2011

Pilgrim Observer Composite.


Here is a composite image of MPC/Round 2 Models 1/100 scale Pilgrim Observer in a fly past of the Planet Mercury (Mariner image). You can view images of the model here.

Sunday, April 24, 2011

Composites





For those of you who have been viewing my web page for awhile may notice that from time to time I enjoy doing occasional composites of my models using Photoshop. That is placing photographs of my models into natural or unnatural settings. Well here are some images of my latest examples. I hope you enjoy them.

First up we have an image of Moebius Models 1/160 scale Orion III Space Clipper from 2001 a Space Odyssey. The image represents the Orion in a blast off accent on its way to an orbiting space station.

Next we have an image of my scratch built Unmanned Soviet Space Probe from 2010 Odyssey II (The Year We Make Contact) flying over The moon Europa, a Galilean satellite of Jupiter. Europa moon surface photo taken by NASA. Europa itself courtesy of God.

After that we have an image of Moebius Models 1/128 scale Seaview from the 60's TV series Voyage to the Bottom of the Sea in an underwater setting. Underwater composites I find tend to be more difficult than they appear. You have to match the object colour to its surroundings and then one has to add a slight blur to everything.

Finally we have an image of Lindberg's 1/200 scale 1950's concept Space Base Space Station.
I sometimes wonder that if the technology to build Space Stations were around in the 1950's if this is in fact what they would have looked like.

Thursday, March 31, 2011

Pilgrim Observer






Here are some images of MPC/Round 2 models 1/100 scale spacecraft The Pilgrim Observer.

From Old Plastic Model Kits"

There was a time when space research was not aimed at the earth's orbit and moon, but at distant planets in our solar system and eventually beyond. Planning went much further than most people are aware. The main limitation was seen as the chemical rocket motor. It could only be fired once and the specific impulse was limited. To overcome these limitations, the United States embarked on a large program to build the nuclear rocket engine. Unlike the nuclear aircraft engine, this program overcame the technical obstacles placed before it was VERY successful. The effort resulted in numerous test engines up through the Phoebes 5000 MW monster, which is still the world's most powerful reactor. The nuclear engines could run at full power for an hour, then be shut down and restarted up to a dozen times or more. Also, the flow of fuel (liquid hydrogen) could be regulated through turbo-pumps to 'throttle' the engine just as one does a car engine. Crew radiation shielding from the engine was less than requirements for cosmic ray shielding. At one point, a KIWI series reactor (KIWI-TNT) was blown up on purpose to test the environmental impact; it was minimal and clean up went quickly. The final result was to be a space rated engine called NERVA, or Nuclear Engine for Rocket Vehicle Application. Before the project was terminated, many vehicles were designed for deep space exploration based on these amazing engines.