Welcome to Night Walkers
Friday, September 28, 2007
Skulls on Mars?
Thursday, September 20, 2007
The X-33 VentureStar
On August 5, 1994, President Clinton issued the National Space Transportation Policy and designated NASA as the Lead Agency for advanced technology development and demonstration of the next generation of RLVs. Three concepts and preliminary designs were prepared independently by: (1) Lockheed Martin Skunk Works, Palmdale, California; (2) McDonnell-Douglas Aerospace, Huntington Beach, California; and (3) Rockwell International Corporation, Space Systems Division, Downey, California.
- demonstrate a reusable cryogenic tank system, including the tanks for liquid hydrogen (LH2) and liquid oxygen (LOX), cryogenic insulation, and an integrated thermal protection system (TPS).
- verify TPS durability, low maintenance, and performance at both low and high temperatures.
- demonstrate guidance, navigation, and control systems, including autonomous flight control of checkout, takeoff, ascent, flight, reentry, and landing for an autonomously controlled space vehicle.
- achieve hypersonic flight speeds (speeds up to Mach 15 or 18,000 km/hr(11,000 mph)).
- demonstrate composite primary space vehicle structures integrated with the TPS.
- demonstrate ability to perform 7-day turnarounds between three consecutive flights (a turnaround is the amount of time required from a takeoff and flight until the vehicle is serviced, refueled, and ready to fly again).
- demonstrate ability to perform a 2-day turnaround between two consecutive flights.
- demonstrate that a maximum of 50 personnel performing hands-on vehicle operations, maintenance, and refueling can successfully accomplish flight readiness for two flights.
- successful interaction of the engines, airframe, and launch (also referred to as takeoff) facility.
- engine performance, thrust, and throttling capability meets specifications.
- operability and control of the X-33's flight control surfaces (canted fins, flaps, ailerons, etc.)
- durability of the metallic thermal protection system during repeated flights.
- performance of the guidance, navigation, and control system.
- performance of primary operations facilities, including takeoff infrastructure.
- automated landing at a designated point on the runway.
- verification of tasks required to service the vehicle on landing and prepare it for next flight in minimal time.
The RLV will fly much like the Space Shuttle. It will take off vertically and land on a runway. However, there are differences between the two vehicles. The RLV will be a means of transport only. It will not be used as a science platform like the current Space Shuttle.
Also, the RLV will be a single-stage-to-orbit spacecraft it does not drop off components on its way to orbit. It will rely totally on its own built-in engines to reach orbit, omitting the need for additional boosters. Unlike the shuttle, the RLV will use a new linear aerospike engine, which looks and runs much differently than the bell-shaped Space Shuttle Main Engine. NASA considered the aerospike engine for the Space Shuttle 25 years ago, but opted to use the Space Shuttle Main Engine, also built by Rocketdyne. The aerospike has been revived and enhanced to power the RLV. The aerospike nozzle is shaped like an inverted bell nozzle. Where a bell nozzle begins small and widens toward the opening of the nozzle like a cone, the aerospike decreases in width toward the opening of the nozzle. The aerospike is 75 percent shorter than an equivalent bell nozzle engine. It is also lighter, and its form blends well with the RLV's lifting body airframe for lower drag during flight. The shape spreads thrust loads evenly at the base of the vehicle, causing less structural weight.
The half-scale X-33 test vehicle will use two smaller test versions of the aerospike, whilet the full-scale RLV will use seven aerospike engines. The X-33 main propulsion system (full system of engines and propellant tanks) consists of two J-2S aerospike engines, one aluminum LOX tank in the front, and two LH2 tanks in the rear for short- and mid-range flights. The vehicle could sustain one engine out at liftoff and still have sufficient power from the remaining engine to continue acceleration and make a safe landing at the intended runway or an abort landing area depending on where the engine out occurred during flight. For the long- range flights an engine out situation could be tolerated approximately 30 seconds after liftoff.
The X-33 was scheduled to complete its first flight by March of 1999. As of early 1999 the projected date for the X-33 rollout was May 1999, with its first flight planned for that July. The program is scheduled to be completed by the year 2000. The baseline test program would include a combined total of approximately 15 flights beginning in July 1999 and concluding in December 1999. The baseline test flight plan includes three short-range, seven mid-range, and five long-range test flights. Actual numbers of test flights to any range may vary due to changing plans and/or actual test flight data evaluation.
Test flights involve: (1) launching the X-33 from a vertical position like a conventional space launch vehicle?this reduces the weight of the landing gear and wheels to only that required to support an unfueled vehicle (baseline dry weight of vehicle is approximately 29,500 kg (65,000 lb) and fueled weight of X-33 is approximately 123,800 kg (273,000 lb)); (2) accelerating the vehicle to top speeds of Mach 15 (15 times the speed of sound or approximately 18,000 km/hr (11,000 mph) and reaching high altitudes up to approximately 75,800 m (250,000 ft); (3) shutting down the engines; gliding over long distances up to 1,530 km (950 mi) downrange of the launch site followed by conducting terminal area energy maneuvers to reduce speed and altitude; and (4) landing like a conventional airplane.
Optimally, the flight test plan to meet Program objectives would involve flights of approximately 160, 720, or 1,530 km (100, 450, and 950 mi). Landing sites meeting the above criteria and providing 3,050 m (10,000 ft) of hard surface are referred to as short-, mid-, and long-range landing sites, respectively. The X-33 Program prefers to land the vehicle on a dry lake bed at least for its first flight in order to have a wider and slightly safer landing area than conventional runways offer. The same philosophy was used for the Orbiter's and most X-planes' first landings.
Silurian Dry Lake Bed near Baker, California is approximately 3000 feet wide and 12000 feet long. The lake bed will be the site of the first landing attempts for the X-33 vehicle. Three flights are scheduled to Silurian Lake that will include vehicle speeds in excess of Mach 3. The flights are scheduled to start in mid 1999.
Michael Army Airfield will be the second landing site for the X-33. This will also be the first downrange runway landing. Michael Army Airfield is part of the Utah Test and Training Range, located south of Salt Lake City. This airfield is located on the eastern boundary of Dugway. The airfield has a 3,960 m (13,000 ft) long by 61 m (200 ft) wide hard surfaced runway. Immediate surrounding terrain is relatively flat. It is a secure facility with a long history of flight operations. The airspace above Dugway Proving Ground is restricted military airspace controlled by Hill Air Force Base which manages and approves use of the Utah Test and Training Range (UTTR). Seven flights are scheduled to Michael with vehicle speeds in excess of Mach 10. Flights are scheduled to start in the latter part of 1999.
Tuesday, September 18, 2007
Living the lie on a secret base
When researching I came across this guy on a forum claiming that he has worked at a secret installation in the past. It makes for interesting reading.
"Im not going to go into great details here as this is a public site. I was forced to sign a security oath that forbids me from discussing the base in details and its functions. And when I say forced, I literally was told "sign this or you dont leave this facility ever"
I will say that generally there are facilities around this nation that have stated publicly what the base does exactly. This from my experience is a complete lie. I have personally witnessed base commanders bring reporters onto base and set up false shows as to say "see this is what we do here"
What was very shocking to me is that some of the hidden secret activities were quite dangerous to the local public. And these activities endangered far more than just a few local farmers. Sometimes events happened that did some damage to the local community and the general public wasnt told.
If you live near any type of military or DoD installation, I urge you to do some research or just use your eyes. If you see reports of higher than normal cancer rates, there's a clue. If you notice that the tree line suddenly stops when approaching a facility, again another clue. These dead zones are clear to anyone that looks but for some reason most dont seem to have their eyes open.
My sister once asked me how if UFO's or 9-11 were real could the govt possibly keep it a secret. Well I lived it, FEAR was the reason. Hell, Im fearful now that the NSA is flagging this posting. Although, Im sure Im aleady on a watch list anyway as Ive voiced my opinions many times over the years. (my wife is deathly afraid Ive made the infamous FEMA list and would be imprisoned immediately upon martial law being declared).
Fear keeps people from talking. And in a society that loves freedom its a real shame that fear will keep dirty secrets from coming outI would also like to state that the fear is constantly reinforced by the govt.
Ill give a few examples...
I would say that on at least 3 occasions I was approached by women in various social outings. They were basically trying to get "close" to me if you catch my drift. Im not talking like James Bond stuff, ie get into my hotel room and snapshot some documents or anything lol. But just really silly obvious attempts to see if I could be compromised.
Sometimes I got the impression that these obvious attempts were done just as a show of force to let me know theyre always watching.
On other occasions there were attempts to probe me for weaknesses that could possibly be exploited. The govt would want to know if you have a gambling problem or have drug or alcohol dependency, or money problems, etc. I had been given chances to join in card games, betting pools, sexual encounters with prositiution rings, and some really oddball activities.
Once I was approached by some (what looked like) high school or young college kids about me getting involved in some counterfeit ID ring operation.
It is possible that some of these attempts to compromise me were in fact real operatives. Others were certainly just the govt testing me. In fact I recall once while waiting for a bump with my clearance status one of the above attempts happening.
It really made me afraid to say anything. I was always afraid any slip of the tongue would net me a visit to Ft. Leavenworth. When these guys would listen in on my phone calls they wouldnt even try and hide it. A few times I distinctly heard a click and another time I could somehow hear an entirely other phone conversation going on between other people.
I dont think full disclosure will ever happen in my lifetime honestly. Not unless the cloak of fear is ever lifted. Its real, its threatening, and it keeps people quiet."
Friday, September 14, 2007
NASA's 'Morphing Airplane'
An artist's rendering shows advanced concepts NASA envisions for an aircraft ofNow this is a strange concept to begin working on. An aerospace vehicle that morphs depending on various flight characteristics. Obviously NASA tell the whole truth and nothing but the truth so this is as they say just an 'advanced concept'.......Yeah Right, we all know that when a project is anounced it has more than likely been in operation for numerous years prior to the announcement.
the future. Called the 21st Century Aerospace Vehicle, and sometimes nicknamed
the Morphing Airplane, the concept includes a variety of smart technologies that
could enable inflight configuration changes for optimum flight characteristics.
Kliper: too many unknowns
Sometimes, we copy each other's problems with mirror-like precision. Here is the latest example.
Until recently no one could doubt the prospects of Russia's reusable space transport system. For some years the Russian Space Agency (Roskosmos) has been talking its head off about the Kliper craft as the system's core. When early this year a tender was announced for developing and manufacturing a spaceship, it was a mere formality. Everybody knew the winner would be the Energiya Rocket and Space Corporation's Kliper project. Its features have been paraded dozens of times, its mock-ups have been on display at shows and exhibitions from Tokyo to Paris to Berlin. The fruit was about to fall from the tree.
Also until recently we knew practically nothing of a similar American project. The Americans intend to build, under NASA's Constellation Program, the reusable Crew Exploration Vehicle (CEV) for missions to the International Space Station and, later to the Moon and Mars.
Overnight everything changed. Late in June, speaking at the Farnborough aerospace show, the Roskosmos leadership suddenly announced that they were suspending the tender and would instead adopt a multi-stage program of creating a space transport vehicle. Now the main emphasis is on the time-tested orbital workhorse, the Soyuz spacecraft. On the American side, everything is tip-top and clear. They have even come up with a name: Orion.
From elementary algebra we know that a linear equation like X + 5 = 10 can be solved when there is only one unknown. The Americans seem to be on good terms with mathematics. According to NASA's interpretation, everything is clear and understandable. If the two aerospace giants - Lockheed Martin and Northrop Grumman - plus Boeing, which all claim leadership of the Constellation Program, are given the 1.1 billion dollars allocated for the development and construction of the spacecraft by 2012, we will get the desired X: the Orion.
For the Russian program, or its new package, it is impossible even to compile a rough equation. Here is a quote from an Internet news briefing held by Roskosmos chief Anatoly Perminov, who on July 24 tried to explain the sudden change in the plans to build a Russian space transport system.
"The year-by year breakdown of research and development costs provided by companies bidding to build a likely ship, in particular the Kliper, exceeds the figures in the Russian Federal Space Program budget for 2006-2015, so the program must be drastically changed.
"In view of the above, after examining the bids, a proposal by the Energiya Rocket and Space Corporation to develop a promising transport system in two or three stages was given preference. Its suggestion for the first stage is to upgrade and modernize the Soyuz spacecraft, which has proved its worth over forty years of operation by being very reliable and relatively cost-effective in taking a crew member to an orbiting station. The modernization effort, in our view, should ensure that the new Soyuz makes not only orbital flights, but also missions to the Moon, making room for new engineering solutions and system tests for use in the next stages of development of a new-generation craft. The results of first-stage work may help us to decide on the type of the next-generation ship, if one is necessary."
Even a cursory glimpse at the quote suggests there are three unknowns involved. The first is money. The part about "breakdown of costs" leads us to understand that no money has been or is available for the Kliper.
Strange. The new spacecraft has been in the news for some time now. Time enough for its full-scale replica to be put on view at the MAKS-2005 air show in Zhukovsky outside Moscow, where it was photographed by dozens of journalists and seen by hundreds of tourists. A bit later, a special government resolution, dated October 22 and numbered 635, approved Russia's Federal Space Program. The Manned Flights subsection explicitly tells us that "... steps are planned to develop a new-generation spacecraft."
It emerges that Energiya and all the rest of them have been working on something which was in no way to be subsidized. Or, if subsidized, then the program had to be "drastically changed."
To my knowledge, Energiya has estimated the cost of the Kliper project at $1 billion. Let us recall, incidentally, the American program's $1.1 billion. But the Federal Program budgeted only one-third of that sum. In other words, a super-modern craft was to have been built without sufficient financing. But I do not think that anyone would ever have managed to develop and build a space transporter for the price of a pair of pantyhose.
The second unknown in this para-mathematical solitaire is the space veteran, the manned Soyuz ship. Why all this fuss with the Kliper if Energiya always had an ace up its sleeve - the Soyuz orbiter - which can easily be passed off as a Lunik? True, upgrading the ship would involve substantial outlays, as an old rule of thumb says about recarving something old into something new.
And the last unknown is the Kliper itself, which will now get a new lease on life "if necessary". This "if" breeds sad thoughts about the prospects for the re-engineered Soyuz and its ability to stride across centuries.
It is clear that developing a Kliper-type reusable spacecraft was attempted on the off-chance that it would be possible to fund it, which is so typical of Russians. But the well-spinned Russian idea failed to catch the attention of both Russian and foreign sponsors.
No one disputes that Russia is a great space power, and no one will ever doubt it as long as we throw out the deadwood of "unknowns" from our programs.
Wednesday, September 12, 2007
'Grey at the window' Video
The images above are analysis I carried out on a video found recently on You Tube by a fellow member of www.ufocasebook.com. It allegedly shows an alien (resembling a Grey) looking through a window of a house before being chased into the nearby woods by the occupants of the home.
Its very strange and after enhancing some stills from the video it is clear to see that there is a shape at the window that resembles a face of some kind.
I think you need to watch the video yourselves before you make up your mind on this so here is the link to the UFO Casebook forum where this video is discussed (Go to page 10/11 of the thread). The You Tube Link is there also.
http://ufocasebook.conforums.com/index.cgi?board=aliens&action=display&num=1174354861
The mysterious TR-3B program
The TR-3B vehicles outer coating is reactive to electrical Radar stimulation and can change reflectiveness, radar absorptiveness, and color. This polymer skin, when used in conjunction with the TR-3Bs Electronic Counter Measures and, ECCM, can make the vehicle look like a small aircraft, or a flying cylinder--or even trick radar receivers into falsely detecting a variety of aircraft, no aircraft, or several aircraft at various locations. A circular, plasma filled accelerator ring called the Magnetic Field Disrupter, surrounds the rotatable crew compartment and is far ahead of any imaginable technology.
Sandia and Livermore laboratories developed the reverse engineered MFD technology. The government will go to any lengths to protect this technology. The plasma, mercury based, is pressurized at 250,000 atmospheres at a temperature of 150 degrees Kelvin and accelerated to 50,000 rpm to create a super-conductive plasma with the resulting gravity disruption. The MFD generates a magnetic vortex field, which disrupts or neutralizes the effects of gravity on mass within proximity, by 89 percent. Do not misunderstand. This is not antigravity. Anti-gravity provides a repulsive force that can be used for propulsion. The MFD creates a disruption of the Earth's gravitational field upon the mass within the circular accelerator. The mass of the circular accelerator and all mass within the accelerator, such as the crew capsule, avionics, MFD systems, fuels, crew environmental systems, and the nuclear reactor, are reduced by 89%. This causes the effect of making the vehicle extremely light and able to outperform and outmaneuver any craft yet constructed--except, of course, those UFOs we did not build.
The TR-3B is a high altitude, stealth, reconnaissance platform with an indefinite loiter time. Once you get it up there at speed, it does'nt take much propulsion to maintain altitude. At Groom Lake their have been whispered rumours of a new element that acts as a catalyst to the plasma. With the vehicle mass reduced by 89%, the craft can travel at Mach 9, vertically or horizontally. My sources say the performance is limited only the stresses that the human pilots can endure. Which is a lot, really, considering along with the 89% reduction in mass, the G forces are also reduced by 89%.
The TR-3Bs propulsion is provided by 3 multimode thrusters mounted at each bottom corner of the triangular platform. The TR-3 is a sub-Mach 9 vehicle until it reaches altitudes above l20,000 feet--then God knows how fast it can go! The 3 multimode rocket engines mounted under each corner of the craft use hydrogen or methane and oxygen as a propellent. In a liquid oxygen/hydrogen rocket system, 85% of the propellent mass is oxygen. The nuclear thermal rocket engine uses a hydrogen propellent, augmented with oxygen for additional thrust. The reactor heats the liquid hydrogen and injects liquid oxygen in the supersonic nozzle, so that the hydrogen burns concurrently in the liquid oxygen afterburner. The multimode propulsion system can; operate in the atmosphere, with thrust provided by the nuclear reactor, in the upper atmosphere, with hydrogen propulsion, and in orbit, with the combined hydrogen\ oxygen propulsion.
What you have to remember is, that the 3 rocket engines only have to propel 11 percent of the mass of the Top Secret TR-3B. The engines are reportedly built by Rockwell. Many sightings of triangular UFOs are not alien vehicles but the top secret TR-3B. The NSA, NRO, CIA, and USAF have been playing a shell game with aircraft nomenclature - creating the TR-3, modified to the TR-3A, the TR-3B, and the Teir 2, 3, and 4, with suffixes like Plus or Minus added on to confuse further the fact that each of these designators is a different aircraft and not the same aerospace vehicle. A TR-3B is as different from a TR-3A as a banana is from a grape. Some of these vehicles are manned and others are unmanned.
Strange satellite image showing black aircraft?
Monday, September 10, 2007
SR-71 Blackbird on Aircraft Carrier!!
Check out this excellent image from Google Earth of an SR-71 on an aircraft carrier in the New York area. Definately something you dont see everyday!
Link: http://maps.google.com/?ie=UTF8&z=19&ll=40.764456,-74.00002&spn=0.000892,0.002682&t=k&om=1
Wednesday, September 5, 2007
Air Force Plans Flight Tests Of Hypersonic Vehicle
The Falcon Hypersonic Technology Vehicle program is exploring high-speed air vehicles designed for rapid, around-the-world reach. Project goals are to develop hypersonic technology for a glided or powered system, as well as advance small, low cost, and responsive launch vehicles.
A Falcon Hypersonic Test Vehicle-1 (HTV-1) is now on the books for a less than one-hour flight in September 2007. Attaining Mach 19 (19 times the speed of sound), the glided air vehicle will briefly exit the Earth's atmosphere and reenter flying between 19 and 28 miles above the Earth's surface. This inaugural voyage of HTV-1 would end in the Pacific Ocean.
The Falcon HTV program is geared to showcase the ability of a craft to attain hypersonic speeds - ranging from 6,000 to 15,000 miles per hour (Mach 9 to Mach 22), and reach altitudes between 100,000 to 150,000 feet. To do so will necessitate an airframe structure designed to survive intense heat and pressure.
There are other partners participating in the demonstration program: NASA, the Space and Missile Systems Center, Sandia National Laboratories and the Air Force Research Laboratory's (AFRL) Air Vehicles and Space Vehicles Directorates.
Work is now underway to build the Falcon HTV-1's flight hardware components. The test vehicle will be integrated at a Lockheed Martin facility in Valley Forge , Pennsylvania.
AFRL's Space Vehicles directorate, located at Kirtland Air Force Base in New Mexico, is specifically focusing on technologies for the glided system and issued a January 25 background release on the hypersonic work. Technologists there are helping to develop a thermal protection system for the HTV structure to withstand 3,000-degree temperatures and extreme exterior pressures - 25 times those experienced by NASA's space shuttle orbiter.
Other critical technology to be investigated in the Falcon HTV work includes an all carbon aeroshell. This outer casing must tolerate crushing pressures and intense heat. To keep the vehicle interior cool, an advanced multi-layer insulation is being fabricated for long duration flights. In addition, researchers are designing tools for enhanced HTV navigation and maneuverability.
A second glided flight is slated for 2008 or 2009. That HTV-2 test would feature a different structural design, enhanced controllability, and higher risk/performance factors during its high-speed journey. Like its predecessor, the system will reach Mach 22 speed, and then finish its one-hour plus mission in the Pacific Ocean.
Also scheduled is a third and final flight of a Falcon HTV. That test shot is planned for 2009 and will be a departure from the previous two demonstrations.
This time the reusable hypersonic glider will lift off from NASA's Wallops Flight Facility, Wallops Island, Virginia.
Screaming out of the area, the HTV-3 would be recovered in the Atlantic Ocean an hour later. In addition, the HTV-3--flying at a maximum Mach 10 speed--would achieve high aerodynamic efficiency and validate external heat barrier panels that will be reusable.
"We have made great progress and are on track for the first glided hypersonic test vehicle flight in 2007," said Russ Partch, Falcon HTV-1 project manager in the AFRL release. "It will enable a revolutionary capability to quickly respond to events anywhere around the world."
The results of the trio of HTV experimental flights are viewed as having a significant impact in the development of future
affordable, adaptable, and responsive military delivery platforms and launch systems.
According to AFRL, the Falcon HTV program is expected--during the next three to four years--to tackle challenges related to hypersonic flight by in-flight validation of technologies while demonstrating operationally responsive space lift.
Story from: http://www.space.com/businesstechnology/060126_darpa_falcon.html