Wednesday, December 26, 2012

The Aeronca 7 Champion


Country of origin  

United States of America

Powerplants

7AC - One 50kW (65hp) Continental A65-8 flat four piston engine driving a two blade fixed pitch propeller.

Performance

7AC - Max speed 161km/h (87kt), cruising speed 128km/h (70kt). Service ceiling 12,400ft. Range 740km (400nm).



Weights

7AC - Empty 325kg (740lb), max takeoff 533kg (1220lb).

Dimensions

7AC - Wing span 10.73m (35ft 2in), length 6.65m (21ft 6in), height 2.13m (7ft 0in). Wing area 15.8m2 (170sq ft).

Capacity  

7 - Pilot and single passenger in tandem.

Production

Approx 10,000 Aeronca Champions (including L-16s and 7200 7ACs) built between 1946 and 1951.

Type  

Two seat light aircraft


History

The Aeronca Champion was a highly popular light aircraft in the USA in the intermediate postwar period, with over 10,000 built.

The Champion was based on the prewar Model K Scout, with which it shares an overall similar configuration, but with tandem instead of side by side seating and a reduced span but increased chord flapless wing.

The first production version of the Champion was the 7AC, with succeeding versions similar except for the powerplant fitted. These versions were the 7BC with a 63kW (85hp) Continental C85-12 or O-190-1 (and built in large numbers for the US Army as the L-16 liaison platform); the 7CC with a Continental C-90-12F; and the 7DC with a Continental C85.

Aeronca sold the production rights of the Champion to the Champion Aircraft Corporation in 1951. Champion Aircraft dropped production of its namesake that year and instead developed the 7EC Traveler with a 67kW (90hp) Continental C90 (which first flew in 1955), 7FC tricycle undercarriage Tri-Traveler and the 110kW (150hp) Lycoming O-320 powered Model 7GCB Challenger, with increased span wing with flaps. The Challenger formed the basis for the Citabria and subsequent Decathlon and Scout, which are described separately under American Champion.

In September 1970 Bellanca acquired the assets of the Champion Aircraft Company and elected to return the Champion to production as the 7ACA Champ. Based on the 7AC, changes included a 45kW (60hp) Franklin 2A-120-B engine in place of the by then out of production Continental, cantilever spring steel main landing gear and modernised interior. Small numbers were built in the early 1970s.

Source: http://www.airliners.net/aircraft-data/

The Aeronca 11 Chief


Country of origin

United States of America

Powerplants

One 48kW (65hp) Continental A-65-8F (11AC), or 63kW (85hp) Continental C-85-8F (11BC/CC), or 67kW (90hp) Continental C-90 (HUL-26).

Performance

Max speed 169km/h (91kt) for the 11AC, 177km/h (96kt) for the 11BC/CC, cruising speed 153km/h (83kt) for the 11AC, 161km/h (87kt) for the 11BC. Service ceiling 10,800ft for the 11AC, 14,500ft for the 11CC. Max initial rate of climb 152m (500ft)/min for the 11AC, 198m (650ft)/min for the 11CC. Range 531km (287nm) for the 11AC, 595km (322nm) for the 11CC.


Weights  

Empty 329-340kg (725-750lb) for the 11AC, 372kg (820lb) for the 11CC. Max loaded 567-612kg (1250-1350lb) for the 11AC, 612kg (1350lb) for the 11CC.

Dimensions

Wing span 11.00m (36ft 1in), length 6.35m (20ft 10in), height 2.08m (6ft 10in). Wing area 16.3m2 (175.5sq ft).

Capacity

Accommodation for pilot and passenger side by side.

Production  

2325 Chiefs built between 1946 and 1951 (including 1867 11AC, 181 11BC, and 277 11CC) plus 154 Pushpaks built between 1958 and 1968.

Type  

Two seat light aircraft


History

The Aeronca 11 Chief, designed by Ray Hermes, was developed at the same time as the tandem seat Model 7 Champion, but it featured a wider cabin for side by side seating. The first flight was made in 1945, but the type was only shown publicly for the first time at the National Air Show in Cleveland in November 1946.
The Chief has a welded steel tube fuselage with fabric covering. A door on each side gives entry to the side by side cabin, and a baggage compartment is located behind the seats. Streamlined wheelpants were available as an option. Except for the fuselage, 80% of the parts are interchangeable with the Model 7 Champion.

The first version of the Chief was the 11AC, powered by a 48kW (65hp) Continental A-65-8F engine, and the Type Certificate was issued September 28 1945. A floatplane version on Edo Floats was certificated on July 22 1947 as the S11AC. The Chief was available in a "Standard" version, or as a fully-equipped "Deluxe" version. In 1947 a "Scout" version was added, which was a bare pilot trainer.
The 11BC had a more powerful 63kW (85hp) Continental C-85-8F engine and a large dorsal fin, and was also available as the float-equipped S11BC. These models were certificated respectively in August 1947 and September 1948.

The third version was the 11CC Super Chief with the same Continental C-85 engine, but with a little more room, improved styling, luxury equipment now included as standard, and some other improvements. The 11CC was certificated in May 1948, and its float-equipped equivalent, the S11CC, in October 1948.
In 1951 Aeronca stopped production of light aircraft, as the market for light aircraft was not profitable anymore and as they had large orders for Korean War equipment to fulfill.

E.J.Trytek acquired the rights for the Model 11, but did not build the Chief themselves. The 11CC was however licence-built in India as the Hindustan HUL-26 Pushpak with a 67kW (90hp) Continental C-90 engine. The first flight was made on September 28 1958, and the type was produced until 1968. A total of 154 were received by Indian flying clubs.

Eventually, Bellanca bought the Model 11 type certificate, and they used the model for developing a new trainer. They rebuilt a standard 11AC to the new model, but after a lengthy test period did not proceed further with the design.

Source: http://www.airliners.net/aircraft-data/

The Aero Boero AB-95/115/150/180


Country of origin

Argentina

Powerplants

AB-95 Standard - One 70kW (95hp) Continental C90-8F flat four driving a two blade fixed pitch prop.
AB-115 Trainer - One 85kW (115hp) Textron Lycoming O-235-C2A.

AB-180RVR - One 135kW (180hp) Textron Lycoming O-360-A1A driving a two blade fixed pitch Sensenich or constant speed Hartzell prop.

Performance

AB-95 - Max speed 204km/h (110kt), cruising speed 170km/h (92kt), long range cruising speed 159km/h (86kt). Range at long range cruising speed 959km (518nm).

AB-115 Trainer - Max cruising speed 169km/h (91kt). Initial rate of climb 669ft/min. Range with max fuel 1230km (664nm).

AB-180RVR - Max speed 225km/h (122kt), max cruising speed 201km/h (108kt). Initial rate of climb 1025ft/min. Range with max fuel 1180km (636nm).


Weights  

AB-95 - Empty 400kg (882lb), loaded 700kg (1543lb).

AB-115 Trainer - Empty 556kg (1226lb), max takeoff 802kg (1768lb).

AB-180RVR - Empty 602kg (1327lb), max takeoff 890kg (1962lb).

Dimensions

AB-95 - Wing span 10.42m (34ft 2in), length 6.91m (22ft 8in), height 2.19m (7ft 2in).

AB-115 Trainer & AB-180RVR - Wing span 10.78m (35ft 5in), length 7.08m (23ft 3in), height 2.05m (6ft 9in). Wing area 17.4m2 (187.4sq ft).

Capacity

Accommodation for one pilot and two passengers, or three/four passengers in initial AB-180 model. Ag aircraft fitted with ventral tank pod (for approx 270 litres/60Imp gal) and spray bars.

Production

Approx 600 of all variants have been built, including over 300 out of a Brazilian Government order for 450 AB-115s for use by aero clubs.

Type  

Family of three and four seat light aircraft


History

Development from the basic AB-95 (which first flew in 1959) has spawned one of the largest families of GA types yet developed in South America.

Versions of the AB-95 include the AB-95 Standard, the AB-95 De Lujo with a 75kW (100hp) Continental O-200A engine, the AB-95A Fumigador ag aircraft with the O-200A engine and fitted for crop dusting or spraying, the AB-115BS air ambulance fitted with a stretcher, the more powerful AB-95B, and the AB-95-115 with a more streamlined engine cowling housing a 85kW (115hp) O-235 engine, and main wheel fairings.

From the AB-95-115 Aero Boero developed the AB-115BS with increased wing span, greater fin sweepback and longer range, and the AB-115 Trainer. Brazil ordered 450 Trainers in the late 1980s for its aero clubs.

The AB-180 first flew in the late 1960s and was offered in three and four seat versions with differing wingspans and a more powerful powerplant than those featured on the earlier AB-95 and AB-115. Developments included the AB-180RV with greater range, reprofiled fuselage and sweptback fin; the glider tug AB-180RVR; the high altitude AB-180 Condor with optional engine turbocharger; AB-180AG agricultural aircraft and the two seat AB-180PSA preselection aircraft for student pilot flight grading. An experimental biplane AB-180SP was also developed. The AB-150RV and AB-150AG have less powerful powerplants than corresponding AB-180 models.

Source: http://www.airliners.net/aircraft-data

The Aermacchi F-260


Country of origin  

Italy

Powerplants

SF-260A & C - One 195kW (260hp) Lycoming O-540-E4A5 flat six piston engine driving a two blade constant speed prop.

Performance

SF-260A - Max cruising speed 345km/h (186kt). Initial rate of climb 1770ft/min. Service ceiling 21,370ft. Range with max fuel 2050km (1107nm).

SF-260C - Max speed 347km/h (187kt), max cruising speed 330km/h (178kt). Initial rate of climb 1790ft/min. Service ceiling 19,000ft. Max range 1490km (805nm).


Weights  

SF-260A - Empty 700kg (1543lb), max takeoff (aerobatic) 1000kg (2205lb), max takeoff (utility) 1102kg (2430lb).

Dimensions

SF-260A - Wing span over tip tanks 8.40m (27ft 7in), length 7.02m (23ft 0in), height 2.60m (8ft 6in). Wing area 10.1m2 (108.5sq ft).

SF-260C - Wing span 8.35m (27ft 5in), length 7.10m (23ft 4in), height 2.41m (7ft 11in). Wing area 10.1m2 (108.7sq ft).

Capacity  

Typical seating for two side by side, plus rear seat capable of seating one adult or two small children.

Production

Over 860 SF-260s have been built (750 by SIAI-Marchetti) of which approximately 170 built for civil customers.

Type  

Two seat trainer and high performance light aircraft


History

The nimble SIAI-Marchetti SF-260 has sold in modest numbers to civil operators worldwide but is one of the most successful postwar two seat piston military trainers.

The SF-260 was designed by famed Italian aircraft designer Stelio Frati (who was responsible for a number of renowned light aircraft designs) in the early 1960s. It was originally flown in 185kW (250hp) Lycoming O-540 powered form by the Aviamilano company as the F-250. However until its takeover by Aermacchi in 1997 SIAI-Marchetti undertook all production (initially under licence, before later assuming full responsibility for the program) of the aircraft as the 195kW (260hp) O-540 powered SF-260. The second aircraft to fly was the first built by SIAI-Marchetti and the first powered by the more powerful version of the O-540. This second prototype first flew in 1966.

The initial civil production models were the SF-260 and SF-260A, and a number were sold in the USA as the Waco Meteor. In 1974 production switched to the SF-260B with improvements first developed for the military SF-260M, including a stronger undercarriage, a redesigned wing leading edge and a taller fin. The B was soon followed by the further improved SF-260C, with increased span wing.

While the SF-260 has been further developed into E and F forms these have been sold to military operators only. The 260kW (350shp) Allison (now Rolls-Royce) 250-B17D turboprop powered SF-260TP meanwhile has been built since the early 1980s, but it too has been sold only to military customers. Nevertheless Italian civil certification was awarded in October 1993, opening the door for possible civil sales.

In civil use the SF-260 is now regarded as something of a classic thoroughbred. Its clean aerodynamic lines, retractable undercarriage and relatively powerful engine guarantee spirited performance.
In 1997 Aermacchi took over SIAI-Marchetti and continues to market the aircraft as the F-260, with low rate production continuing against military orders.

Source: http://www.airliners.net/aircraft-data/

The AEA Explorer

Country of origin

Australia


Type  

Multirole utility transport


Powerplants

350R - One 260kW (350hp) Teledyne Continental TSIO-550-E3B turbocharged and fuel injected flat-six piston engine driving a three-blade Hartzell propeller.

500T - One 447kW (600shp) Pratt & Whitney Canada PT6A-135B turboprop driving a four-blade propeller

Performance

350R - Max cruising speed 278km/h (150kt). Initial rate of climb 750ft/min. Takeoff run 366m (1200ft). Service ceiling 25,000ft. Max range with reserves 1852km (1000nm). Endurance over 3hr.

500T - Cruising speed 333km/h (180kt). Initial rate of climb 1000ft/min. Takeoff run 366m (1200ft). Service ceiling 25,000ft. Max range with reserves 1759km (950nm).

Weights

350R - Empty 1360kg (3000lb), max takeoff 2177kg (4800lb).

500T - Empty 1723kg (3800lb), max takeoff 2812kg (6200lb)

Dimensions

350R - Wing span 14.43m (47ft 4in), length 9.68m (31ft 9in), height 4.72m (15ft 6in). Wing area 18.36m2 (197.6sq ft).

500T - Wing span 14.43m (47ft 4in), length 10.13m (33ft 3in), height 4.72m (15ft 6in). Wing area 18.36m2 (197.6sq ft).

Capacity

350R - Seating for nine (including pilot) in a passenger configuration. Cargo volume 7.08m3 (250cu ft).

500T - Seating for eleven (including pilot) in a passenger configuration. Cargo volume 7.08m3 (250cu ft).

Production

One 350R, later converted to 500T (by Feb.2002)


History

The AEA Explorer 350R is a nine-place Australian utility aircraft developed by Aeronautical Engineers Australia Research Pty Ltd (AEA). It is designed to fill a market gap between the Cessna 206 Stationair and the much larger Cessna 208 Caravan utility singles.

AEA's managing director Graham Swannell first began looking at a new utility aircraft in the late 1980s, and initially considered developing a stretched and more powerful Cessna 206 conversion which would have been covered by a supplemental type certificate. But by 1993 Swannell had started design work on an all new aircraft, a 10 seater powered by an eight cylinder 300kW (400hp) Textron Lycoming IO-720. This design then evolved to become the Explorer 350R, a nine-seater powered by a Teledyne Continental TSIO-550 flat-six.

The 350R flew for the first time on January 23 1998. Apart from its TSIO-550 engine driving a three blade prop, design features include a metal frame fuselage with a carbonfibre shell, conventional all metal wings and tail surfaces and retractable undercarriage. The main undercarriage retraction system is uncommon - the legs, which are made from fibreglass, extend further downwards before crossing each other below the fuselage with the wheels coming to rest in pods on the opposite side of the fuselage - thus not intruding into the main cabin.

The aircraft's basic configuration is optimised for its intended utility roles, with a high mounted, braced wing, rectangular and constant section, flat floor cabin, and large cabin windows.

The Explorer 350R will not be built in series, but is the proof-of-concept (POC) prototype for a family of utility aircraft. The 350R prototype was converted to the 500T prototype, powered by a 600shp Pratt & Whitney PT6A-135B turboprop, and the first flight as such was made on June 9 2000. The 500T has seating for eleven (including the pilot) in a passenger configuration, and will be the entry level aircraft for the Explorer. A second production version will be the 500R, a 600hp Orenda OE-600A piston engine powered version of the 500T. A 2.21m (7ft 3in) stretched version is planned, the Explorer 750T, which will seat 17 (including the pilot), and will be powered by a 750shp Pratt & Whitney PT6A-60A turboprop.

On May 20 1999 the 350R left Australia for a promotional tour of the USA, and will now be further developed and taken into production in the United States by Explorer Aircraft Inc, located in Jasper, Texas.

Source: http://www.airliners.net/aircraft-data/


The AASI Jetcruzer



Country of origin

United States of America


Type  

Business and utility transport


Powerplants

One rear mounted 1172kW (1572shp) Pratt & Whitney Canada PT6A-66A turboprop driving a five blade constant speed Hartzell propeller.

Performance

Max cruising speed 576km/h (318kt). Service ceiling 30,000ft. Max range at economical cruising speed with reserves 2574km (1391nm).

Weights

Max takeoff 2495kg (5500lb).

Dimensions  

Wing span 12.85m (42ft 2in), length approx 10.5m (34.4ft).

Capacity  

Typical accommodation for six including pilot. Can be configured for ambulance, cargo and other utility work. Optional aft lavatory.

Production

450 - 3 were built.
500 - by November 2001, 2 had been converted from 450s, 1 new one was built, and 197 were on order.

Basic unit price (2001) $US1.495.000

History

The innovative Jetcruzer 500 is designed to be a high speed low cost single engine corporate turboprop and is the product of California based Advanced Aerodynamics and Structures Inc (AASI).

The Jetcruzer 500 is based on the smaller, unpressurised Jetcruzer 450. Early design work for what would become the Jetcruzer 450 began in 1983. Construction of an Allison 250-C20S powered prototype began in 1988. It flew for the first time on January 11 1989.

The preproduction prototype first flew April 1991, and the first production standard Jetcruzer 450 on September 13 1992. When FAA Part 23 certification was granted on June 14 1994 the Jetcruzer became the first aircraft in the world to be certificated as spin resistant.

AASI elected not to place the 450 into production and instead focused its efforts on the pressurised 500. Initial work was on the 500P, which featured a modest 25cm (10in) fuselage stretch, but AASI instead decided to enlarge the design further. The definitive Jetcruzer features a 1.83m (6ft) fuselage stretch over the 450 (increasing cabin length by 90cm (3ft), plus a significantly more powerful PT6A66 turboprop driving a five (rather than three) blade prop, pressurisation to 30,000ft, an airstair entry door on the right hand side and additional cabin windows.

First flight of the prototype 500 (the modified preproduction prototype 450) was in August 22 1997, followed by the second prototype (the modified production 450) on November 7 1997.
Other notable Jetcruzer 500 design features include its canard configuration (which allows the main wing to be positioned further aft than normal, so the wing spars do not intrude into the cabin), lack of flaps (reducing pilot work load and manufacturing costs and saving weight), and optional EFIS avionics. Like the 450 the 500 will be certificated as spin resistant. The fuselage is made from composites while the wing and canard are aluminium.

On February 8 2002, AASI announced that it was taking over the Mooney assets, and that the name Mooney would be used for the combined companies. Headquarters, development, and marketing would remain at AASI's facility at Long Beach in California, but production of the Jetcruzer would be at Mooney's Kerrville, Texas plant.

The company is also working on the Stratocruzer 1250, a 13 place twin WilliamsRolls FJ-44 powered light corporate jet development.



Source: http://www.airliners.net/aircraft-data/

Russian stealth aircraft

Prototype stealth fighter of the Russian army will be released to the public for the first time at the MAKS-2011 air show, opening today, 16-8, in the suburbs of Moscow.

Stealth fighter T-50 flight test at the outskirts of Moscow. Photo: RIA

Generation stealth aircraft Sukhoi T-50 is considered to be a pillar in the near future of the Russian Air Force, as line fighter Mikoyan MiG-29 and Sukhoi Su-27 became obsolete.

T-50 is the first fighter of the Russian army completely new design since the late 1980s. After officially put into operation, it will be the first stealth aircraft of the Russian Air Force is equipped with outstanding features.

Like the famous F-22 aircraft of the United States, T-50 is capable of flying at supersonic speeds, the engine thrust vector, as well as high-tech flight control system.

Despite the relative shape like F-22, but military experts around the world confirm that T-50 is completely new aircraft, level design, excellent manufacturing of aviation engineer Russian space.

The first T-50 prototype took off for the first time at the airport Komsomolsk-on-Amur, Siberia in January. Currently, Russia has had two samples of the aircraft and are doing the test flight near Moscow.

Expected to start in 2015, the Russian Air Force will buy 200 T-50 and some exports to the countries potential customers. Currently, India is also contributing capital to Russia to participate in the research, manufacture stealth fighter based on the T-50.

At the international air show MAKS 2011 held in Zhukovskiy, a suburb of Moscow, next to the famous aircraft was known to the world, for the first time, the Russian defense industry will formally introduce T -50 with the public at home and abroad.



China's stealth aircraft

China continued to test stealth fighter

The J-20 stealth fighter of China, which caused a stir public opinion recently, has taken off in the 27th test flight in Sichuan Province, southwest China.


Some netizens have to photograph the test on 15/8 in the city of Chengdu.

According to Xinhua, this is the 27th test flight of the J-20

J-20 stealth fighter is the 5th generation, developed for the Chinese navy by the Chengdu Aircraft Industrial Group.

J-20 took off for the first time in January this year.

J-20 can be equipped with long-range missiles as well as aerial refueling.

J-20 can launch cruise missiles and carrying heavy weapons.

Deputy commander of the Chinese Air Force, General He Weirong, claimed that the J-20 will be staffing the country in the Air Force from 2017 to 2019

The aircraft can not be seen with the naked eye of Russia

5th generation fighter aircraft Russia is Su T-50 stealth technology application will prevent aircraft from being detected even with the naked eye.

F-35 stealth fighter of the U.S

Plasma stealth technology

Traditional stealth technology that many countries are using, the most typical is the latest generation fighters such as the F-117, B-2, F-22 and J-20 in China, which is using the angular structure scattering of electromagnetic waves in all directions combined with new materials and special coating to absorb radar waves, reduce infrared radiation emitted by the engine ...

However, for the Sukhoi PAK FA T-50, Russian technology developed entirely new "plasma stealth" or also known as "active stealth technology."

Process technologies make use of ionized air to reduce radar reflection cross section (Radar cross section RCS). Ionized gas will cover the entire aircraft and absorb the electromagnetic energy of the radar waves, which makes it difficult to detect aircraft from enemy air defense systems.

Camouflage stealth technology

However, Russia does not want his stealth aircraft before the enemy's radar invisibility but even with the naked eye and optical devices. That prompted Russia to develop a completely new stealth technology "e-camouflage" by the use of special materials.

The surface of the imaging plane will be in real time, in the environment it is operating. Through advanced computer and use special materials, the camera will project the image onto the surface of the plane to make it look like the sky and the surrounding terrain, meant to put on PAK FA a hidden shirt.

Technology "e-camouflage" This used to be in the public domain in the movie "Die Another Day", when the car Aston Martin's 007 invisible to the naked eye.

T-50 will apply technology "electronic invisible".

Meanwhile multifunctional fighter PAK FA T50 can perform tasks takeoff ground attack during the day, it would not need to attack at night like some American bombers nowretired as the F-117, and F-35.

Invisibility can help PAK FA T50 gain advantage in the war when the enemy pilot can not see it with the naked eye. However, the F-35 is equipped with modern photoelectric sensor system, which allows pilots to look away hundreds of kilometers to display heat emitted by a PAK FA.

Whether the PAK FA T50 will have the technology "e-camouflage" or not, it is important that the United States deployed a strong force of the 5th generation fighter odds have the ability to respond to the potential challenges such as PAK FA in Russia or China's J-20.

America will need a large enough number of generation fighters in order to reduce losses, against potential competitors and have the advantage of numbers in a war with a large air power.

Duma is considering the impact of the stealth fighter export it to other countries. Apart from India, Russia, the PAK FA can sell arms to Iran if sanctions of the United Nations to be removed, or to Arab countries if the U.S. refused to sell F-35, as well as Venezuela, Vietnam, Indonesia, Malaysia , and perhaps even China, as the PAK FA are rated higher than the J-20 is still unknown.






Price $ 715 million aircraft

The aircraft Aviatr looks like unmanned aircraft are mobilized to Afghanistan. However, this 715 million dollar machine designed to fly over Saturn's largest moon Titan.

Aviatr-like unmanned aircraft in Afghanistan

By the end of the mission, the aircraft weighs right 120 kg will lower the height and try to land the giant dunes of Titan.

To do this, Aviatr will be equipped with a horizontal camera extremely sensitive. This camera will be able to turn round to take a comprehensive picture of the clouds above Titan.

On aircraft equipped with ultra-sensitive cameras to capture 3D images of the atmosphere and surface Titan

"We believe that Titan particularly suited Aviatr: gravity of the moon is relatively low but the atmosphere thick. That means that the small aircraft and lightweight as Aviatr can fly in the air longer, "said Jason Barnes, the authors designed Aviatr said.

Aviatr fuel from a generator powered by plutonium-238Aviatr fuel from a generator powered by plutonium-238

Unlike hot air balloon - a solution has also been proposed to explore Titan, Aviatr will allow scientists to precisely control the height of it, and built a library of 3D images of the surfaceand weather Titan. Aviatr will use fuel from a generator powered by plutonium-238. When sending data back to Earth, the plane will switch to sleep mode to conserve energy.

Titan is larger than our Moon and even Mercury. Its surface temperature is about -178 to 178 degrees C.

$ 715 million of Aviatr including a missile and a multi terrain rack to the aircraft can be landed on the surface of Titan

Jason Barnesh currently working at the University of Idaho. But the idea of Aviatr could not round final funding approval of NASA, but Mr. Barnes still hope that this project will get the attention from the other side. Barnes said a satellite is heavier than air is the best way to explore the planet Titan's thick atmosphere, and a hot air balloon, though cheaper, but it will be useless.






AVIATR: An Airplane Mission for Titan

An artist's conception of AVIATR, an airplane mission to the second largest moon in our solar system: Titan. Credit: Mike Malaska 2011


It has been said that the atmosphere on Titan is so dense that a person could strap a pair of wings on their back and soar through its skies.

It’s a pretty fascinating thought. And Titan – Saturn’s largest moon – is a pretty fascinating place. After all, it’s the only other body in our solar system (besides Earth, of course) that has that type of atmosphere and evidence of liquid on its surface.

“As far as its scientific interest, Titan is the most interesting target in the Solar System,” Dr. Jason W. Barnes of the University of Idaho told Universe Today.

That’s why Barnes and a team of 30 scientists and engineers created an unmanned mission concept to explore Titan called AVIATR (Aerial Vehicle for In-situ and Airborne Titan Reconnaissance). The plan, which primarily consists of a 120 kg plane soaring through the natural satellite’s atmosphere, was published online late last month.

The goal of the plane concept – which according to Barnes can serve as a standalone mission or as part of a larger Titan-focused exploration program – is to study the moon’s geography (its mountains, dunes, lakes and seas), as well as its atmosphere (the wind, haze, clouds and rain. Did you know that Titan is the only other place is our solar system where it rains?)

AVIATR is composed of three vehicles: one for space travel, one for entry and descent into Titan, and a plane to fly through the atmosphere. AVIATR, estimated to cost $715 million, would not prevent other missions from occurring on Titan, Barnes said. Instead, it would supplement the science being done by other projects.


“The science that AVIATR could do complements the science that can be accomplished from both orbiting and landed platforms,” the article stated.

Unfortunately, it seems like the plane concept won’t be happening anytime soon.

That’s because Titan didn’t make the National Research Council’s “Decadal Survey” – a prioritization of future planetary missions. (Read more about the survey in this Universe Today post.)
“Titan was deferred to another decade,” Barnes said.

But, he hopes to continue to build support for AVIATR so that it can get onto the next decadal survey in 2020. “We certainly had a lot of interest from people. We are breaking the paradigm that a balloon was the right way to go to Titan,” Barnes said.

So, why send an unmanned plane to study Titan’s atmosphere?

“Titan is the best place to fly an airplane in the whole solar system. We can go when and where we want,” Barnes said, adding that when compared to Earth, there’s four times more air and seven times less gravity on Titan. “A balloon is stuck in the wind.”

According to the article:

“A balloon entrained in primarily zonal winds near the equator would have no mechanism by which to travel to the polar regions to observe lakes and shoreline processes. Even if it were possible to get there, it is not clear that it would be desirable to send a balloon to the poles where Titan’s most violent meteorological activity takes place. AVIATR is both able to fly to the poles and is sufficiently robust to survive there.”

Mission poster for AVIATR. Credit: Mike Malaska

There’s also this issue: A shortage of plutonium-238.

“The radioactive decay of plutonium-238 provides the heat that powers RTGs, which can power spacecraft where there is insufficient sunlight for solar panels to operate. NASA is presently investing in a new type of RTG, called the ASRG,” the article stated. “A traditional hot-air balloon will not work on Titan with an ASRG owing to its lower heat production. In contrast, the AVIATR mission is specifically enabled by the use of ASRGs. The power density (in Watts per kilogram) and longevity of the ASRG allow an electrically-powered aircraft to fly on Titan.”

A plane could also find potential landing spots for future exploration. And, “since we are flying, we fly west the whole time so we can stay on the day side of Titan,” Barnes said.

That daylight would also help AVIATR collect photographic data during its travels and, according to Barnes, when it’s time to downlink that information, the plane would conserve energy by gliding through the air.
“And in doing so, we can also sample of bunch of altitude ranges,” Barnes said. “We are sampling the whole time.”

The plan seems interesting enough, but it’ll be quite a while before any data from the prospective mission would be coming back to Earth. If the plan is accepted (the earliest being 2020), the project would still have to be built, then once completed it would take 7 1/2 years to reach Titan. Once there, the mission would take about a nominal Earth year to study.

“I now realize that it’s a career-long project,” Barnes said to Universe Today. “The plan at this point is to keep this in the forefront of people’s minds and take whatever new ideas that people suggest and try to improve its prospect for selection.

Source: http://www.universetoday.com/92286/aviatr-an-airplane-mission-for-titan/





Sunday, December 23, 2012

Virgin Galactic SpaceShipTwo: Aircraft space




Virgin Galactic's SpaceShipTwo is a space plane built to carry passengers to the region bounded by outer space. The aircraft was developed based on SpaceShipOne was designed by Burt Rutan

The company is planning for the first flight in the summer after the auction service provider to become the only astronaut.
The trip will last about 3.5 hours to adjacent regions of space outside the earth and then come back. Customers will have to pay about $ 200,000 per person. This 18m long aircraft can carry six passengers plus two pilots.

According to statistics from the website of Virgin Galactic's had about 430 people booked. In October last year, the company also announced an agreement with NASA flight Rent a contract worth $ 4.5 million. Virgin Galacticco plans to start operations in the U.S. spaceport in New Mexico in 2013.

RQ-170 Sentinel: unmanned stealth aircraft




U.S. military aircraft were used for reconnaissance missions.

Unmanned Vehicles (UAV) developed by Lockheed Martin and the U.S. Air Force (USAF) to grant use to the CIA in 2007. This aircraft is not known until 2009, when the surface of the plane surface. There is very little information disclosed about the features of plane by CIA security mechanisms. Images are distributed on the net that this is an airplane with no tail and bat wings. Board RQ design also implies that the UAV was not armed.

According to information that the Sentinel was used to monitor the organization of f Osama bin Laden in Pakistan Navy SEAL mission in May 2011. This unmanned aircraft also cause noisy on January 9 last year when the Iranian government media published an RQ-170 was shot down while flying over their airspace.

U.S. side has officially announced the unmanned aircraft that Iran shot down last week due to technical problems and the crash landing. Iranian television news reports informed the government will try to test unmanned aircraft systems in the U.S. and now the final step unlocking software of the aircraft.

Terrafugia Transition: Cars with wings




Terrafugia Transition is a plane that also functions as a car and be able to be a perfect replacement in the future. This winged car can transform from a car to a plane in less than a minute with a wing spread that the driver does not need to get out of the car.

Terrafugia Transition is a group of MIT aeronautics engineers built with two seats made ​​of carbon, 100-horsepower engine, was developed and the first test flight in the U.S. since 2006. With a car, it can reach speeds of more than 100km / h, or flying at the speed of 180km / h in a 800km radius and using unleaded petrol.

Except for the inevitable still blocked the road, aircraft price 297 000 USD is an ideal choice for those who just like to drive just like flying on the same media.

The aircraft manufacturers have overcome a huge obstacle to the Committee in July 2011 when the national road traffic safety of the United States through the use of this aircraft on the road. The aircraft also been named in Time Magazine in the list of the 50 best inventions of 2010. The company also plans to begin selling in late 2012.

Antonov AN-225 Mriya: Aircraft carrying the Space Shuttle




Antonov AN-225 Mriya is the heaviest aircraft and the world's largest current account. 6 motor and chamber up to 250 tons, the aircraft can carry up to 50 cars at a time.

The AN-225 was designed to transport the Buran shuttle program Soviet space travel. The first was delivered in 1988, while the first two have not been completed since the federal Soviet collapse in 1991. Currently AN-225 is under the management the Antanov Airline companies of the Ukraine, used for freight purposes. According Kostiantyn Lushakov Antanov CEO, wanted to build the 2nd AN-225 needs at least $ 300 million and take three years to complete.

The aircraft have been a number of organizations used for humanitarian relief after natural disasters. In 2010, the AN-225 is used to transport large equipment in the earthquake in Haiti, in 2011 was 140 tons of relief supplies and other equipment to Japan.

WP-3D Orion: hurricane hunting aircraft




The Lockheed WP-3D Orion aircraft, also known as hurricane hunting aircraft of the National Hydrometeorological Center USA (NOAA), is responsible for flying high in the center of the storm with up to7500m to collect data such as the path of the storm, storm intensity.

Was first introduced in 1976, so far the world's only 2 the newest P-3D Orion. Aircraft jet engine is equipped with a full range of equipment such as radar, sensors, data recording system to record information about pressure, meteorological and environmental information such as the state of the sea and marine life. In addition to the tasks detect hurricanes, P-3 is involved in a number of international research programs. One of them is the study of the possibility of following the oil spill disaster in the Gulf of Mexico in 2010. Data on air quality, the environment around the bay has been recorded and sent to the center.

In Hurricane Irene this past September, two P-3 collected information to help NOAA predicted landfall in North Carolina and the scanning direction of the storm on the East coast.
We have proposed budget cuts of the American Meteorological Center budget including the storm forecast up to 40% may interfere with the aircraft's future.

Erickson S-64: overhead crane




The aircraft crane Erickson S-64 is a dual-engine helicopter can carry a weight of up to 11.5 tonnes. This is also the first helicopter not interfere pilots in the observed objects are transported.

Cranes on the S-64 was manufacturing firms Sikorsky in 1962, 30 years after the copyright was acquired by Erickson production. So far Erickson has 1350 changes in the helicopter. S-64 was known to the world since the Vietnam War and later generations of U.S. military aircraft to the CH-54A "Tarhe" collectors identify aircraft, aircraft damage. A total of 380 of enemy aircraft were recovered, save for the army up to $ 240 million.

Since entering the market in 1969, this aircraft was involved in building some of the world's most famous works. In 1975, it was used to raise the top of the CN Tower in Toronto, tallest tower in the world can not stand at that time. In 1993, the aircraft was contracted to move the Statue of Liberty sits atop Capitol Hill in Washington DC S-64 also plays an important role in global energy. Since 1971, it has flown more than 12,000 miles to transport high voltage electricity poles across North America.

Bombardier 415: "mega water Gao"




Bombardier 415 is a water bomber duality of Canada, the aircraft is designed specifically for the fire from the air.

In the U.S. aircraft shell is also known as super large, Bombardier 415 debuted in 1994, and currently has 76 units are in service at 18 organizations in 10 countries. The aircraft can take up an amount of more than 7m3 in round 12s while surfing on the water at high speeds. It can spray water 9 times within 1 hour, containing 66 m3 of water to extinguish the fire or fires. Bombardier 415 can also be used in relief, search and rescue, surveillance and movement of workers.

On January 12, the aircraft reached the milestone of 200,000 flight hours and over 6 million m3 of water injection since entering the market two decades ago. The unit price of an aircraft is not disclosed, but in March 2011, Bombardier announced the company has sold 4 415 with a total of about $ 162 million.

Airbus A300-600ST: "White Whale"




"White whale" of Airbus is the world's largest cargo aircraft, is designed to transport can be a whole other plane. Dubbed the plane super load by "white whale" up to 56m in length and can carry loads up to 47 tons of over 900 nautical miles.

Herd 5 "white whale" is located under the management of Airbus with the first launch in 1995. This is a unique design that includes the world's largest chamber and the nose of the aircraft can be opened to bring the goods into the massive size.

"White Whale" is designed to meet the needs of the manufacturer Airbus. Parts of the aircraft at the company are manufactured by companies of four European countries: France, Germany, England and Spain. The body and wings are "white whale" transported to the assembly at the factory. "White Whale" is also used to transport spacecraft from the Italian to Kennedy space stations in Florida, rental transportation, and are also used for military transport aircraft, chemical tanks, also the work French art.


Ten of the world's most dangerous aircraft


Fatal aircraft accidents happen more and more in the world. Based on statistical indicators death (the number of flying hours / number of fatal accidents), The Business Week ranked the safety of a number of aircraft currently in use around the world.

Based on data of the insurance consultancy Ascend, BusinessWeek has ranked the safest aircraft not currently in use around the world. Standing on the number of fatal accidents, eliminate terrorist-related accident, the aircraft is considered to be the most dangerous is the Boeing 737 JT8D. Here is a category 10 safest aircraft in the world, the level of danger descending numerical order.

1.Boeing 737 JT8D 



The aircraft crashed in 8/2008 in Kazakhstan, not long after the European Union banned the Itek Air's flights to Asia because of its planes do not meet safety standards, with 68 people killed.

According to BusinessWeek, for every 507,500 hours of flying Boeing 737 JT8D happened a deadly plane crash. So far, the version of "oldest" of their Boeing are still airlines exploitation in poor countries.