Orion-NASA

Friday 14 February 2014

OPPO-N1

The Mobile With Rotating Camera


OPPO was the first in the world to release a 13-megapixel camera smartphone. With the N1, we are once again realizing new possibilities in smartphone photography. Introducing the world’s first smartphone with a rotating camera.
The revolutionary rotating camera features a 206° rotation, and will securely lock at any angle. No matter what angle you choose, having just one amazing camera means that front facing shots are finally just as good as back facing shots.




The N1 camera features a rotation of 206° and will firmly lock in position at any angle. This was determined as the optimum range of motion for the lens after thousands of adjustments and tests, with each degree serving an exact purpose. By fine tuning every degree, we were able to create the ultimate smartphone camera experience.



N1 features a 5.9-inch Full HD screen. The immersive display of the OPPO N1 is definitely large, but its size is overshadowed by the incredibly clear and sharp delivery of your content. The ultra-sensitive multi-touch panel in the OPPO N1 supports input from fingertips, gloves and styluses for unprecedented freedom over how you control your device.



O-Click lets you remotely operate the N1 camera even when you’re away from the device. Simply position the N1 and step back to include everything you want to capture. If you misplace your device, find it by setting off an alarm on the phone. O-Click fits on your keychain and supports a range of up to 15 meters, staying connected to your OPPO N1 via Bluetooth (BLE).



O-Touch is an entirely new way of using your smartphone. A 12 cm2 rear touch panel makes one handed use for the large OPPO N1 screen comfortable and easy. With O-Touch you can scroll, tap, or snap photos – all without your fingers blocking the display.

Tuesday 11 February 2014

'നോമാന്‍ഡി'

നോക്കിയയുടെ ആന്‍ഡ്രോയ്ഡ് ഫോണ്‍



ഈ വര്‍ഷം ടെക്നോളജി ലോകം കാത്തിരിക്കുന്ന ഏറ്റവും വലിയ പുറത്തിറക്കല്‍ നോക്കിയയുടെ ആന്‍ഡ്രോയ്ഡ് ഫോണ്‍ എന്നതാണ്. പുറത്തിറക്കല്‍ ഈ മാസം ഉണ്ടാകുമെന്ന് വാള്‍ സ്ട്രീറ്റ് ജേണല്‍ റിപ്പോര്‍ട്ട് ചെയ്യുന്നത്. നോക്കിയയുടെ ആന്‍ഡ്രോയ്ഡ് ഫോണ്‍ ഫെബ്രുവരി 24ന് ആരംഭിക്കുന്ന ബാഴ്സിലോനയിലെ ലോക മൊബൈല്‍ കോണ്‍ഗ്രസില്‍ നോക്കിയ പ്രഖ്യാപിക്കുമെന്നാണ് റിപ്പോര്‍ട്ട്. 


ഒരു കാലത്ത് മൊബൈല്‍ വിപണിയിലെ മുന്‍നിരക്കാരായിരുന്ന നോക്കിയയ്ക്ക് മുന്‍കാല പദവി തിരിച്ചുപിടിക്കാന്‍ സഹായിക്കുന്നതായിരിക്കും ഈ ഫോണ്‍ എന്നാണ് വിലയിരുത്തപ്പെടുന്നത്.
ആന്‍ഡ്രോയ്ഡിനെ നിരന്തരം എതിര്‍ത്തിരുന്ന നോക്കിയ, മൈക്രോസോഫ്റ്റിന്റെ വിന്‍ഡോസ് ഫോണ്‍ പ്ലാറ്റ്‌ഫോമാണ് സ്മാര്‍ട്ട് ഫോണുകള്‍ക്കായി ഉപയോഗിക്കുന്നത്. ഇതിനു പുറമേ നോക്കിയയുടെ ഫോണ്‍ബിസിനസ്സ് ഏറ്റെടുക്കാനുള്ള നടപടിയുമായി മൈക്രോസോഫ്റ്റ് മുന്നോട്ടുപോകുകയാണ്.




വിന്‍ഡോസ് ഇന്‍റര്‍ഫേസില്‍ ഒരു ആന്‍ഡ്രോയ്ഡ് ഫോണ്‍ എന്നതായിരിക്കും നോക്കിയയുടെ ആന്‍ഡ്രോയ്ഡ് ഫോണ്‍ എന്നാണ് പുതിയ റിപ്പോര്‍ട്ട്.
നേരത്തെ EVLeaks എന്ന വെബ് സൈറ്റ് ഫോണിന്‍റെ ചിത്രങ്ങള്‍ പുറത്തുവിട്ടിരുന്നു. 


ഗൂഗിള്‍ രൂപപ്പെടുത്തുന്ന ആന്‍ഡ്രോയ്ഡ് പ്ലാറ്റ്ഫോമല്ല നോക്കിയ ഉപയോഗിക്കുക. ആമസോണ്‍ അതിന്റെ കിന്‍ഡ്ല്‍ ഫയര്‍ ടാബുകളില്‍ ഉപയോഗിച്ചതുമാതിരി, സ്വന്തംനിലയ്ക്ക് പരിഷ്‌ക്കരിച്ച ആന്‍ഡ്രോയ്ഡ് വേര്‍ഷനാകും നോക്കിയ ഉപയോഗിക്കുക. 'നോമാന്‍ഡി' എന്ന പേര് തന്നെ അതിന് ഉദാഹരണമാണ്. നോക്കിയ എക്സ് എന്നായിരിക്കും പുതിയ ഫോണിന്‍റെ പേര് എന്നാണ് വേര്‍ജ് പ്രസിദ്ധീകരിച്ച വാര്‍ത്തയില്‍ പറയുന്നത്.


എന്നാല്‍ ആന്‍ഡ്രോയ്ഡ് അപ്ലികേഷന്‍ സ്റ്റോറായ ഗൂഗിള്‍ പ്ലേ ഈ ഫോണില്‍ ലഭിക്കാത്തത് ഫോണിന് തിരിച്ചടിയാകുമോ എന്ന ആശങ്ക നോക്കിയയ്ക്കുണ്ട്. അതിനാല്‍ പല പ്രിയ ആന്‍ഡ്രോയ്ഡ് അപ്ലികേഷനുകളും ഇന്‍ബില്‍ട്ടായി നോക്കിയ നല്‍കുമെന്നാണ് അറിയുന്നത്. 

വിലകുറഞ്ഞ സ്മാര്‍ട്ട്‌ഫോണുകളുടെ നിരയിലുള്ളതാകും നോക്കിയയുടെ ആന്‍ഡ്രോയ്ഡ് ഫോണെന്ന് വെര്‍ജിന്റെ റിപ്പോര്‍ട്ട് പറയുന്നു.
'ആഷ' പരമ്പരയിലെ ഫോണുകളുടെ വിലനിലവാരമായിരിക്കും നോമാന്‍ഡിക്കും. ആഷ ഫോണുകളെ അപേക്ഷിച്ച് കൂടുതല്‍ ആപ്പുകള്‍ അതില്‍ ലഭ്യമാകും. അതായത് 4ജിബിവരെ ഇന്‍റേണല്‍ സ്റ്റോറേജ് ആയിരിക്കും ഫോണില്‍ ഉണ്ടാകുകയെന്നാണ് സൂചന, റാം 512 എംബിയായിരിക്കും എന്നാണ് അറിയുന്നത്.

Sunday 28 April 2013

ELIICA


The Eliica (or the Electric Lithium-Ion Car) is a battery electric vehicle prototype or concept car first shown in 2004 and designed by a team at Keio University in Tokyo, led by Professor Hiroshi Shimizu. The 5.1 m (17 ft) car runs on a lithium-ion battery and can accelerate from 0–100 km/h (62 mph) in four seconds (faster than the Porsche 911 Turboat the time). In 2004, the Eliica reached a speed of 370 km/h (230 mph) on Italy's Nardò High Speed Track. The team's goal is to exceed 400 km/h (250 mph), breaking the record set by today's street-legal gasoline-powered vehicles.




Called the Eliica - short for Electric Lithium-Ion battery Car - this radical 800bhp eight-wheeler from Japan is proof that electric vehicles can be fast and fun to drive, too. Boasting a four-second 0-60mph sprint and seven-second 0-100mph time, the Eliica is faster than a Porsche 911 Turbo.

So what is it like on the road? In this world exclusive, we took the controls to find out. As soon as you climb into the snug cockpit, you realise this car is built for speed. It's more than five metres long, shaped like a bullet and carries its batteries, software and motors in a narrow chassis bed, giving it the lowest centre of gravity of any prototype we've come across.

In tests, the Eliica has recorded a top speed of 370kph (230mph), although its inventor Hiroshi Shimizu claims it could clear 400kph (250mph) in the right conditions. "When you're dealing with technology thought by most to be slow, heavy and lacking range, you must do better than any supercar," he said.

At our drive at Keio University near Tokyo, we punched the 'D' button on the dash, pointed the car down the road and flattened the gas pedal. With a faintly audible whirr of eight 100bhp in-wheel motors, the 0-60mph sprint was smooth, effortless, quiet - and surreal. The mind-boggling acceleration was on a par with that of a 500bhp GT racing car. Yet the lack of a transmission meant there were no jerky cog swaps as we were thrust back in our seat by an incredible 0.8Gs.

With that ultra-low centre of gravity, the car handles surprisingly well, and has virtually no body roll or nose-dive. It turns in sharply with well weighted steering through the front four wheels, and gives adequate feedback. And it does not feel as big or as heavy as its length and 2,400kg kerbweight suggest.

The only downsides, apart from the tiny cockpit, are that it takes 10 hours to recharge, and a production version would cost £170,000. To bring Shimizu's research back to the future, he needs a major firm's financial power behind him and the whole electric car movement.

Key specs

* Batteries charged from mains
* Styling echoes Citroen DS's





DESIGN DETAILS

The Eliica weighs 2,400 kg (5,300 lb) and seats the driver and three passengers. The body was tested in a wind tunnel. The front doors open forward and the rear doors open upward like wings. The car's platform contains 4 tracks of 80 batteries, which make up one third of the vehicle's cost. They currently require about 10 hours of recharging at 100 volts from empty to full charge, and can be easily charged off a residential power grid.
The car has eight wheels to improve traction, and they are smaller than normal passenger vehicles, so it can be lower to the ground for better aerodynamics and stability. Each of the wheels has a 60 kW (80 hp) electric motor, giving a 480 kW (640 hp) eight wheel drive which can tackle all kinds of road surfaces. The four front wheels steer. The electric motors mean that the Eliica can deliver a smooth acceleration free from gear shifts of about 0.8 g. Each wheel contains a disc brake and employs a regenerative brake system to recover energy.
There are currently (as of 2005) two versions of the Eliica: a Speed model and an Acceleration model. The Speed model is made to challenge gasoline-based records and has a top speed of 370 km/h (230 mph) with a range of 200 km (120 mi). The Acceleration model is made for the street and has a top speed of 190 km/h (120 mph) with a range of 320 km (200 mi).
The estimated cost of development was in excess of US$320,000. Once the team receives corporate sponsorship, they plan to produce at least 200 units. As of early 2007, the projected price was ¥30,000,000 JPY (aboutUS$255,000).
On December 19, 2005, then-Prime Minister of Japan Junichiro Koizumi tested this vehicle in a 10-minute ride to theJapanese Parliament. In 2006, the car was tested by Shintaro Ishihara, the governor of Tokyo, as well as by Naruhito, Crown Prince of Japan.






Friday 15 March 2013



F-35






The Lockheed Martin F-35 Lightning II is a family of single-seat, single-engine, fifth generation multirole fighters under development to perform ground attack, reconnaissance, and air defense missions with stealth capability.[7][8] The F-35 has three main models; the F-35A is a conventional takeoff and landing variant, the F-35B is a short take off and vertical-landing variant, and the F-35C is a carrier-based variant.


The F-35 is descended from the X-35, the product of the Joint Strike Fighter (JSF) program. JSF development is being principally funded by the United States. The partner nations are either NATO members or close U.S. allies. It is being designed and built by an aerospace industry team led by Lockheed Martin. The F-35 carried out its first flight on 15 December 2006.

The United States plans to buy a total of 2,443 aircraft to provide the bulk of its tactical airpower for the U.S. Air Force, Marine Corps and Navy over the coming decades. The United Kingdom, Italy, Netherlands, Australia, Canada, Norway, Denmark, and Turkey are part of the development program; Israel, Singapore and Japan may also equip their air services with the F-35.

An F-35 wind tunnel testing model in theArnold Engineering Development Center's 16-foot transonic wind tunnel




The F-35 Lightning II joint strike fighter program is a different program than it was four years ago, the F-35 program executive officer said here March 12.
In a speech at the McAleese/Credit Suisse Defense Programs Conference at the Newseum, Lt. Gen. Christopher C. Bogdan told attendees that he and his predecessor, Navy Vice Adm. Dave Venlet, worked with Lockheed-Martin and Pratt & Whitney to reform the problem-plagued development program.
“Lockheed-Martin and Pratt & Whitney have been doing a pretty good job over the last few years of stepping up and making those kinds of changes that the government needs for this program to succeed,” the general said.
The aircraft’s development has been rocky, Bogdan acknowledged. A redesign of the short takeoff and vertical landing system in 2004 led to delays and added $6 billion to the cost of the development program, he said.
“Then, in 2009, we somehow managed to drive the train off the tracks on this program,” Bogdan said.
The program breached the Nunn-McCurdy Act, which requires that programs exceeding certain parameters in costs and scheduling appeal to Congress to avoid cancellation.
Venlet led the program through the appeal process, the general said, and “basically gave us a great gift.” The appeal led to an extra 30 months being tacked onto the development schedule and provided $6 billion in additional development funds.
“Anybody that gets three more years and $6 billion better be able to get a program across the finish line,” Bogdan said.
Since then, he said, the program has been making slow and steady progress and is on track, particularly for two significant deadlines — 2015, when the Marine Corps is scheduled to have combat-ready aircraft; and 2017, when development is scheduled to end.

F-35B's thrust vectoring nozzle and lift fan






F-35 cockpit and instrument panel mock-up


“Those two dates are extremely important,” Bogdan said. “If I don’t get to those two dates or I don’t reach the finish line there, then we will continue to produce airplanes that don’t have the capability that the warfighter needs.”
Some of the program changes have been painful, the general said, but were necessary. For example, until 2010 the program was operating without an integrated master schedule, so it was difficult to track the systemwide effects of a change in any part of the program. The schedule has been built, and now tracks about 16,000 items, he said. It’s a small thing that makes a big difference in how a program is managed, he noted.
“We can actually track each of those events and see how they affect the end timeline,” Bogdan said.
His predecessor introduced a more radical change in the engineering process, the general said. Previously, design reviews were conducted by the program office, he said.
“Well, I have a good program office, but I don’t have the resources, nor do I have the expertise that the entire Department of Defense has when it comes to building airplanes,” Bogdan said.
Design review boards are now chaired by government executives from throughout the Defense Department who are seasoned engineers with experience developing successful aircraft programs, he said.
“And they draw on the expertise of all the people underneath them at those organizations to help us decide, technically, ‘Are we ready to move forward?’” he added, noting that the change has paid great dividends.
The general said the program’s affordability is his leading concern. The development program ends in 2017, he said, and is about 90 percent complete, with about $6 billion left in the budget.
“That last 10 percent is the real hard 10 percent,” Bogdan said. “So, what I have told the enterprise is, relative to development, we have no more time, and we have no more money.”
This requires a change in mindset, the general said. Additional expenses have to be offset by a reduction elsewhere, and that, he said, may mean a reduction in end capability.
“That has profound implications for the warfighter. I can honestly tell you that the warfighter does not like me standing up saying that,” Bodgan said.
“There will come a point in time when the enterprise and the warfighters will come back to me and say, ‘Oh no, General Bogdan, that is not what we want you to do. That is too painful for us,’” he said. “Maybe they’ll give me more money and more time, but I will not take the first step in asking for more money and more time. I will try and finish what I’ve promised to finish, given the resources I have.”
F-35 production is “the shining star” of the program, the general said. About 30 aircraft are being built each year, he said, and the cost per unit has come down with each successive low-rate initial production, or LRIP, lot. Between LRIP 4 and LRIP 5, there was a 4-percent decrease in build costs, Bogdan said — a trend he said he believes will continue until per-unit costs approach the original 2001 estimate of $69 million.
“I think we can get there,” he said. “Lockheed-Martin and Pratt & Whitney are doing a pretty good job of coming down that cost curve. They’re getting more efficient in their production line [and] their quality is going up, … and that is a good thing, because I promise you the one thing that our partners care most about is how much this airplane’s going to cost.”
Eight nations have committed to participate in the development program, and another three may buy F-35s, with nearly 3,000 aircraft expected to be produced.
With such a large order and so many partners invested in the aircraft, it’s essential to keep costs down to avoid what Bogdan called the “death spiral,” something he said he’s seen kill off many programs.
The death spiral is when increasing costs lead to a reduction in the number of units purchased, which in turn leads to further per-unit cost increases, and so on.
“I don’t think that’s the fate of this program,” Bogdan said. “But the proof is in the pudding, and we have to continue to see Lockheed-Martin and Pratt & Whitney investing in making the production line more efficient, squeezing the costs out, and getting the unit cost of this airplane down. I think they can do it, but we have to wait and see.”
Production costs are only part of the puzzle, however. About 70 to 80 percent of any program’s costs are in the long-term operation and sustainment phase, the general said.
What’s unique about the F-35 is that the Defense Department has never had to estimate the costs of a 50-year aircraft life cycle, he said. Adding to the complications of producing such a cost estimate is that the department hasn’t had an aircraft program this large since World War II, Bogdan said.
“So, lots of airplanes over a very long period of time, with inflation added in, you can understand how the (Office of the Secretary of Defense) guys come up with a number like $1.1 trillion,” he said. “That’s an astronomical number; it’s based on a lot of assumptions. I’m not saying that that’s a bad number; I’m just saying we need to take that number with a grain of salt.”
What he does know, he said, is that action must be taken soon to reduce the F-35′s long-term sustainment costs. Without it, the general said, a time will come when the services decide that the aircraft is no longer affordable.
“So we have to start doing things today,” Bogdan said.
He said there is already interest from industry in a competitive bidding process to produce, deliver and operate support equipment and pilot and maintenance training centers, administer the logistics and information technology systems and manage the global supply chain.
“The other thing is we’ve got to work on the reliability and the maintainability of the airplane,” he said, a process he described as “Whack-a-Mole.”
“You’ll take care of those first 10 or 20 cost drivers in reliability and maintainability, and then the next 20 will show up,” he explained. “You keep doing that until you get to a point where the reliability and maintainability of the airplane is up where you expected it to be, and in the long term, you can reduce the costs on the airplane.”
Bogdan said recent criticisms about technical issues and allegations of limited aft visibility are ill-informed. “I don’t lose sleep at night over the technical issues on this program,” he said.
There are known solutions for all of the known issues with the aircraft, Bogdan added.
“We have yet to fly a single air-to-air engagement with another F-35 or another airplane,” he said. “The airplane’s not ready to do that. We’re still doing basic training (and testing) on the airplane. So for someone to assess that the visibility behind the airplane is such that it will ‘get gunned down every time,’ (is) a little premature.”
Bogdan summarized his expectations:
“We are trying to instill a level of discipline in this program such that there are no surprises — we have predictable outcomes (and) when we have problems, we have ways of solving those problems,” he said. “(This is) very hard to do on a very big, complex program that has lots and lots of decision-makers (and) lots and lots of pots of money, but I think that’s an absolute necessity to get the program moving in the right direction.”


Tuesday 12 March 2013


HMMWV (Humvee®)






The High Mobility Multipurpose Wheeled Vehicle (HMMWV), commonly known as the Humvee, is a four-wheel drive military automobile produced by AM General. It has largely supplanted the roles formerly served by smallerjeeps such as the M151 14-short-ton (230 kg) MUTT, the M561 "Gama Goat", their M718A1 and M792 ambulance versions, the CUCV, and other light trucks. Primarily used by the United States military, it is also used by numerous other countries and organizations and even in civilian adaptations. The Humvee's widespread use in the Persian Gulf War helped inspire the civilian Hummer automotive marque.



Wherever you see American troops around the world, you see HMMWVs (Humvees) in action. Even around the U.S., in natural disasters such as floods, hurricanes and tornadoes, you'll see HMMWVs when the National Guard is at work.
Although the HMMWV has been in production since 1985, its design is still as revolutionary today as it was when engineers began initial concepts in 1979. The final design met military requirements to replace numerous types of aged vehicles and to keep up with swift moving tanks. The Army wanted durability, mobility and reliability. The unique geometry of the truck provides these qualities. No other light tactical vehicle in the world approaches the HMMWV's capabilities or cost effectiveness.
That doesn't mean today's HMMWVs are the same as those first produced. The HMMWV is a dynamic vehicle with changes and improvements continually added. For instance, thorough corrosion resistance has been added and most components have been upgraded, including the move to a larger 6.5-litre diesel engine. From day one, system developers have continually found new users for the flexible HMMWV. Initially introduced with a 1½-ton payload capacity, increased payload requirements to carry various systems have led to Expanded Capacity Vehicles with payloads up to 5,100 lbs. and gross vehicle weight rating (GVW) up to 12,100 lbs.
As we move well into the 21st century, the workhorse HMMWV is being called on to carry new sophisticated communications and weapons systems. The ongoing story of this rugged truck will continue to unfold as new users are found and new missions require its use.



FEATURES & Design

Its 15 configurations (cargo/troop carriers, weapons carriers, ambulances and shelter carriers) share a common engine, chassis and transmission, with 44 interchangeable parts that are used in more than one position. That means fewer training hours are necessary for the mechanics who will maintain it. Its simplified supply, maintenance and logistics system — essentially one set of common parts for 15 configurations — means lower life-cycle costs which saves tax dollars.
HMMWVs are maintainable, reliable and survivable. They meet all of these requirements while incorporating new standards of reliability for combat vehicles. They score high on Reliability, Availability, Maintainability and Durability (RAM-D) requirements and specifications. During initial production tests, the new vehicle proved to be nearly twice as durable as the Army required.
High ground clearance is a prerequisite for superior mobility. The 16-inch ground clearance of the HMMWV is an engineering feat considering that the vehicle stands only 72 inches high. Full-time four-wheel drive, independent suspension, steep approach and departure angles, 60 percent slope-climbing, 40 percent side slope and 60-inch water-fording capabilities combine with the high ground clearance to make the HMMWV an exceptional off-road vehicle.
The M998 A0 series has a curb weight of approximately 5,200 lbs., a payload of 2,500 lbs. (GVW 7,700 lbs.), and a 6.2 liter V-8 diesel engine with a three-speed automatic transmission. The current comparable model, the M1097A2, weighs only 700 lbs. more but can carry almost twice the payload at 4,400 lbs. (GVW 10,300 lbs). It has a 6.5-liter V-8 diesel with a four-speed automatic transmission. The current production Expanded Capacity Vehicle (ECV) model M1113 has a payload of 5,100 lbs. That is over 2 ½ tons, or very nearly the M1113's own weight of 6,400 lbs. The M1113 has a turbocharged 6.5-liter V-8 diesel. The up-armored variant M1114 is produced by AM General with the armor package installed by O'Gara Hess and Eisenhart.



Design

The HMMWV has a low profile (six feet tall), a wide stance (seven feet wide) and is 15 feet long. These proportions contribute to a stable, road-hugging truck that is very difficult to roll over. This contrasts to the old M151 Jeeps that were considered unstable.
The HMMWV is constructed on a steel frame with boxed frame rails and five cross members constructed from high-grade alloy steel. Once the substructure is assembled, E-coating is applied to provide additional corrosion protection.
The aluminum body reduces weight and provides resistance to corrosion. Aluminum body panels are riveted and bonded together with technologically-advanced adhesives to provide additional strength. The body is designed to flex to accommodate off-road stresses.
The AM General-designed geared hub assembly in the power train doubles the torque to each wheel in the hub of the wheel. This also helps achieve 16 inches of ground clearance, far more than any other vehicle in its class. The use of a double A-arm independent suspension front and rear, coil springs and hydraulic double-acting shock absorbers gives the HMMWV unsurpassed mobility. Four-wheel disc brakes are mounted inboard against the sides of the differentials both of which are located up, between the frame rails, protecting them from impact and debris. Torque-biasing differentials allow the vehicle to continue to move forward as long as any one wheel has traction.
This unique configuration of components along with military 37 x 12.5 radial tires with low-profile runflat devices allows the HMMWV to go places that no other wheeled vehicle in U.S. or foreign military service could go. Some HMMWVs are equipped with an optional central tire inflation system (CTIS). This enables the operator to adjust tire pressure from the driver's seat "on the move" to adapt to changing terrain conditions for greater off-road mobility.
The M1097A2 series features a 6.5-liter Optimizer 6500 diesel engine built by AM General's subsidiary, General Engine Products. It is coupled to a four-speed automatic transmission and full-time four-wheel drive transfer case to provide the HMMWV with exceptional performance. (See specifications) The vehicle can reach speeds of more than 70 mph.
The truck utilizes a 12/24-volt electrical system and has a 25-gallon fuel tank. It has power-assisted hydraulic disc brakes and power steering.
The vehicle has either a 1 + 1 or 2 + 2 seating, depending on the model, on each side of the drive train, which is elevated, allowing the differentials to be raised. This, along with the geared hubs, contributes to high ground clearance. The location of the crew on each side of the drive train also allows for a low center of gravity.


At A Glance

TypeUnarmored: Light Utility Vehicle
Armored: Light Armored Car
Place of origin United States of America
Service history
In service1984–present
Production history
ManufacturerAM General
Unit costUnarmored: $65,000
Armored: $140,000
Produced1984–present
Specifications
Weight5,200–5,900 lb (2,359–2,676 kg) curb weight
Length15 ft (4.57 m), wheelbase 10 ft 10 in (3.30 m)
Width7 ft 1 in (2.16 m)
Height6 ft (1.83 m), reducible to 4 ft 6 in (1.37 m)

Main
armament
see text
Engine8 Cyl. Diesel 6.2 L (380 cu in)
or 6.5 L (400 cu in) V8 turbo diesel
6.5 L V8 turbo diesel: 190 hp (142 kW) @ 3,400 rpm / 380 lbf·ft (515 N·m) @ 1,700 rpm
Transmission3-speed automatic
SuspensionIndependent 4x4
Fuel capacity25 U.S. gal (95 L)
Speed55 mph (89 km/h) at max gross weight
Over 70 mph (113 km/h) top speed


Monday 11 March 2013


SR-71 Blackbird







Having served in the United States Air Force for 20 years, I have marveled at the supreme flying machine called the SR-71...


The Lockheed SR-71 "Blackbird" was an advanced, long-range, Mach 3+ strategic reconnaissance aircraft. It was developed as a black project from the Lockheed A-12 reconnaissance aircraft in the 1960s by Lockheed andSkunk Works. Clarence "Kelly" Johnson was responsible for many of the design's innovative concepts. During reconnaissance missions the SR-71 operated at high speeds and altitudes to allow it to outrace threats. If a surface-to-air missile launch was detected, the standard evasive action was simply to accelerate and outfly the missile.
The SR-71 served with the U.S. Air Force from 1964 to 1998. Of the 32 aircraft built, 12 were lost in accidents, though none to enemy action. The SR-71 has been given several nicknames, including Blackbird and Habu, the latter in reference to an Okinawan species of pit viper. Since 1976, it has held the world record for the fastest air-breathing manned aircraft, a record previously held by the YF-12.





I served for five years in the 9th Strategic Reconnaissance Squadron (SAC) at Beale Air Force Base in Marysville, California. My job was to maintain, inspect, launch and recover the SR-71 Blackbird. From the moment I found out I was to be assigned to the secret Blackbird, to the day I left the organization, it was a love affair to last a lifetime. Each and every launch was a sight to behold. The awesome fact that I was about to launch the worlds fastest air-breathing and highest flying aircraft in the world redefined, to me, the meaning of responsibility. Hello, and welcome to the SR-71 web page. My name is Leland Haynes and I am a retired USAF Master Sergeant. I served on the Blackbird from 1969 to 1974. Just as my tenure with the the 9th SRW was about to end, I was informed we were to make a New York to London speed record attempt. My aircraft (#64-17972) was selected for the speed run based on reliability records of the plane. In August of 1974, I arrived at Farnborough England to receive the aircraft as it landed. My assistant Crew Chief was to launch the plane out from Beale AFB in California.....








FEATURES


General characteristics

Crew:                   2 (Pilot and Reconnaissance Systems Officer)
Payload:              3,500 lb (1,600 kg) of sensors
Length:               107 ft 5 in (32.74 m)
Wingspan:           55 ft 7 in (16.94 m)
Height:               18 ft 6 in (5.64 m)
Wing area:          1,800 ft2 (170 m2)
Empty weight:    67,500 lb (30,600 kg)
Loaded weight:  152,000 lb (69,000 kg)
Max. takeoff weight: 172,000 lb (78,000 kg)
Powerplant:        2 × Pratt & Whitney J58-1 continuous-bleed afterburning turbojets, 34,000                          lbf (151 kN) each
Wheel track:      16 ft 8 in (5.08 m)
Wheelbase:        37 ft 10 in (11.53 m)
Aspect ratio:       1.7



Performance

Maximum speed:       Mach 3.3[86][87][N 5] (2,200+ mph, 3,530+ km/h, 1,900+ knots) at 80,000 ft (24,000 m)
Range:                      2,900 nmi (5,400 km)
Ferry range:              3,200 nmi (5,925 km)
Service ceiling:          85,000 ft (25,900 m)
Rate of climb:           11,810 ft/min (60 m/s)
Wing loading:           84 lb/ft² (410 kg/m²)
Thrust/weight:           0.44



Dimensions:
Overall: 18ft 5 15/16in. x 55ft 7in. x 107ft 5in., 169998.5lb. (5.638m x 16.942m x 32.741m, 77110.8kg)
Other: 18ft 5 15/16in. x 107ft 5in. x 55ft 7in. (5.638m x 32.741m x 16.942m)
Materials:
Titanium
Physical Description:
Twin-engine, two-seat, supersonic strategic reconnaissance aircraft; airframe constructed largley of titanium and its alloys; vertical tail fins are constructed of a composite (laminated plastic-type material) to reduce radar cross-section; Pratt and Whitney J58 (JT11D-20B) turbojet engines feature large inlet shock cones.

Wingspan: 55'7" 
Length: 107'5" 
Height: 18'6"
Weight: 170,000 Lbs


SR-71 timeline

Important dates pulled from many sources.
  • 24 December 1957: First J58 engine run.
  • 1 May 1960: Francis Gary Powers is shot down in a Lockheed U-2 over the Soviet Union.
  • 13 June 1962: SR-71 mock-up reviewed by Air Force.
  • 30 July 1962: J58 completes pre-flight testing.
  • 28 December 1962: Lockheed signs contract to build six SR-71 aircraft.
  • 25 July 1964: President Johnson makes public announcement of SR-71.
  • 29 October 1964: SR-71 prototype (AF Ser. No. 61-7950) delivered to Air Force Plant 42 at Palmdale, CA.
  • 7 December 1964: Beale AFB, CA announced as base for SR-71.
  • 22 December 1964: First flight of the SR-71 with Lockheed test pilot Bob Gilliland at Air Force Plant #42.
  • 21 July 1967: Jim Watkins and Dave Dempster fly first international sortie in SR-71A, AF Ser. No. 61-7972, when the Astro-Inertial Navigation System (ANS) fails on a training mission and they accidentally fly into Mexican airspace.
  • 3 November 1967: A-12 and SR-71 conduct a reconnaissance fly-off. Results were questionable.
  • 5 February 1968: Lockheed ordered to destroy A-12, YF-12, and SR-71 tooling.
  • 8 March 1968: First SR-71A (AF Ser. No. 61-7978) arrives at Kadena AB, Okinawa to replace A-12s.
  • 21 March 1968: First SR-71 (AF Ser. No. 61-7976) operational mission flown from Kadena AB over Vietnam.
  • 29 May 1968: CMSgt Bill Gornik begins the tie-cutting tradition of Habu crews neck-ties.
  • 3 December 1975: First flight of SR-71A (AF Ser. No. 61-7959) in "Big Tail" configuration.
  • 20 April 1976: TDY operations started at RAF Mildenhall, United Kingdom with SR-71A, AF Ser. No. 61-7972.
  • 27–28 July 1976 : SR-71A sets speed and altitude records (Altitude in Horizontal Flight: 85,068.997 ft (25,929.030 m) and Speed Over a Straight Course: 2,193.167 miles per hour (3,529.560 km/h)).
  • August 1980: Honeywell starts conversion of AFICS to DAFICS.
  • 15 January 1982: SR-71B, AF Ser. No. 61-7956, flies its 1,000th sortie.
  • 21 April 1989: SR-71, AF Ser. No. 61-7974, was lost due to an engine explosion after taking off from Kadena AB. This was the last Blackbird to be lost, and was the first SR-71 accident in 17 years.
  • 22 November 1989: Air Force SR-71 program officially terminated.
  • 21 January 1990: Last SR-71, AF Ser. No. 61-7962, left Kadena AB.
  • 26 January 1990: SR-71 is decommissioned at Beale AFB, CA.
  • 6 March 1990: Last SR-71 flight under SENIOR CROWN program, setting four speed records en route to Smithsonian Institution.
  • 25 July 1991: SR-71B, AF Ser. No. 61-7956/NASA #831 officially delivered to NASA Dryden Flight Research Center at Edwards AFB, CA.
  • October 1991: NASA engineer Marta Bohn-Meyer becomes the first female SR-71 crew member.
  • 28 September 1994: Congress votes to allocate $100 million for reactivation of three SR-71s.
  • 26 April 1995: First reactivated SR-71A (AF Ser. No. 61-7971) makes its first flight after restoration by Lockheed.
  • 28 June 1995: First reactivated SR-71 returns to Air Force as Detachment 2.
  • 28 August 1995: Second reactivated SR-71A (AF Ser. No. 61-7967) makes first flight after restoration.
  • 2 August 1997: A NASA SR-71 made multiple flybys at the EAA AirVenture Oshkosh air show. It was then supposed to perform a sonic boom at 53,000 feet (16,000 m) after a midair refueling, but a fuel flow problem caused it to divert to Milwaukee. Two weeks later, the pilot's flight path brought him over Oshkosh again, and there was, in fact, a sonic boom.
  • 19 October 1997: The last flight of SR-71B, AF Ser. No. 61-7956 at Edwards AFB Open House.
  • 9 October 1999: The last flight of the SR-71 (AF Ser. No. 61-7980/NASA 844).
  • September 2002: Final resting places of aircraft #956, #971, and #980 are made known.
  • 15 December 2003: SR-71, AF Ser. No. 61-7972, goes on display at the Smithsonian National Air and Space Museum's Steven F. Udvar-Hazy Center at Washington Dulles International Airport in Chantilly, Virginia.



Saturday 9 March 2013


Oshkosh M-ATV


THE VEHICLE THAT ANSWERS THE URGENT NEED.



The Oshkosh® MRAP All-Terrain Vehicle (M-ATV) is the high-mobility, high-protection medium tactical vehicle specifically engineered for treacherous environments. Derived from the Medium Tactical Vehicle Replacement (MTVR) platform, the M-ATV is a Mine Resistant Ambush Protected (MRAP) vehicle that incorporates the TAK-4® independent suspension system to provide proven, durable, best-in-class mobility. A battle-proven armor configuration provides survivable crew protection as the M-ATV maneuvers over the most grueling terrain.
Each Oshkosh M-ATV variant provides the wheel travel, payload capacity, side slope stability, vehicle durability, extreme mobility and necessary protection needed in an armored fighting vehicle. It’s proven for harsh terrains, proven to save lives, proven to accomplish missions and is supported by Oshkosh throughout its entire life-cycle.





FEATURES


The M-ATV utilizes the MTVR chassis and TAK-4 suspension with the Plasan designed armored hull developed for the Northrop Grumman/Oshkosh JLTV.[8] The V-shaped Plasan armored hull offers protection for the occupants from IED attacks while the centrally inflated run-flat tires allow the M-ATV to travel at least 30 miles at 30 mph even if two tires lose pressure. The vehicle can also take a 7.62 mm round to its engine oil/coolant/hydraulic system and continue to drive for at least one kilometer. The Stat-X engine fire suppression system provides for further survivability.[citation needed] The Tak-4 suspension is coil sprung and fully independent, and offers 16 inches of travel. The M-ATV's roof mounted turret is capable of mounting weapons such as an M240 machine gun, a Mk 19 grenade launcher, an M2 Browning machine gun, or a BGM-71 TOW anti-tank guided missile launcher. The roof weapons can be operated either from the turret by person or remotely inside the cabin with a CROWS remote weapon system. The M-ATV also features modern vehicle safety systems such as Traction control and anti-lock brakes in addition to modern creature comforts such as an HVAC system and power outlets for charging portable electronic devices. Unique among MRAP vehicles are the M-ATV's rear-hinged, aka, suicide doors.






      Oshkosh M-ATV

  
TypeMine-Resistant Ambush Protected
Place of origin United States of America
Service history
Used by United States of America
 Republic of Poland
 United Arab Emirates
WarsWar in Afghanistan
Production history
DesignerOshkosh / Plasan
Designed2009
ManufacturerOshkosh Corporation
Unit cost$470,000+
Produced2009
Number built8,108 on order
Specifications
WeightCurb weight: 27,500 lb (12,500 kg)
Gross weight: 32,500 lb (14,700 kg)
Length246.8 inches (6,270 mm)
Width98.1 inches (2,490 mm)
Height105 inches (2,700 mm)
Crew4+1 gunner

ArmorPlasan composite
Main
armament
1× 7.62 mm (.308 in) M240 machine gun,
1× 40 mm Mk 19 grenade launcher,
1× .50 in (12.7 mm) M2 Browningheavy machine gun, or
1× BGM-71 TOW anti-tank guided missile launcher (not in operational use; MMV prototype only)
Engine7.2 liter inline-6 Caterpillar C7turbodiesel
370 bhp; 925 lb-ft
Power/weight25 hp/ton
Payload capacity4,000 pounds (1,800 kg)
TransmissionAllison 3500SP, 6-speed automaticwith manumatic shifting
Suspension4x4, TAK-4 independent suspension
Operational
range
320 miles (510 km)
Speed65 miles per hour (105 km/h) (electronically limited)