Pasotti F.6 Airone

Designed by Stelio Frati and built by Legnami Passoti, the F.6 Airone is a four-seat low wing twin engine monoplane with dual controls.

A cabin monoplane with two Lycoming engines.

First flown on 13 July 1954, the prototype was powered by two 90 hp Continental C90-12Fs.

Engines: two 90 hp Continental C90-12F
Wingspan: 34 ft 9 in
Wing area: 163.6 sq.ft
Length: 23 ft 9.5 in
Empty weight: 1984 lb
Loaded weight: 3196 lb
Max speed: 198 mph
Cruise: 168 mph
Service ceiling: 21,325 ft
Range: 714 mi

Partenavia P-68

P.68 Observer

The aircraft was designed by Professor Luigi Pascale, professor of aeronautics at Naples University, and his influence over the marketing department is there to see in the P68B’s very clean aerodynamic shape. Six place, powered by two 200hp Lycoming 10-360’s, with room for 400lbs of passenger baggage. The aircraft is designed for optimum aerodynamic efficiency, and this com¬bined with a simple but robust struc¬ture and its fixed undercarriage are factors that have endeared it to operators, who range from outback freight carrying outfits to third levels and executive users. The aerodynamic streamlining is demonstrated in the fuel economy; at optimum performance at 65 percent power (160 kts) the P68B can get through close on 900 miles at a fuel flow rate of some 15 gallons an hour. Entry to the aircraft is by a single door on the port side; simple enough for your average passenger but some¬what small to load any freight. A baggage door is also provided on the starboard side.

The P.68 Victor first flew in May 1970 with two 200-hp (149-kW) 10-360 engines as the prototype of a six/seven-seat lightplane. The type has an unusual appearance, with a racy fuselage and swept fin/rudder assembly married to fixed tricycle landing gear (with attractive speed fairings) and a straight wing and tailplane.

The first production P-68 Victor featured a six-inch fuselage stretch and higher gross weight among modifications developed as a result of field and customer-acceptance trials.

With the Victor established in production and further development, Partenavia then collaborated with a West German company, Sportavia-Putzer, in the development of a patrol and observation version.

In 1980, turbocharging was added for a slight increase in speed and a significant boost in service ceiling.

The Observer has a new forward fuselage incorpo¬rating a Plexiglas nose that offers forward and downward fields of vision comparable with those of a helicopter. The first Observer flew in West Germany during February 1976, and aircraft emerged from the Italian production line from July 1980. Since that time small but useful sales have been made to several police and para-military air arms. The Italian police use the type with the ATAL video surveillance system developed in France by Aérospatiale.

The P-68C features a lengthened nose, oleo-type nosewheel strut, an integral fuel tank in each wing and other refinements. Some featured a crew door.

Partenavia P68C

The certification RAI A-365 came from Registro Aeronautico Italiano for the P-68B, P-68C, and P-68C-TC.

Partenavia P68C

AD’s include “Extended safe life” kit 68-038 (Spar Caps replaced) and Max takeoff weight increase kit P68-051.

The Partenavia P.68R’s main wheels fold into the fuselage fairings with a speed gain averaging about eight knots. The version provided so little improvement over the standard that it never went into production.

Several versions of the P.68 are offered for military and paramilitary roles, including the P.68 Observer twin-piston-engined observation/surveillance aircraft, the AP.68TP-300 Spartacus for coastal patrol, troop transport, and medevac with two 240 hp Allison 250-B17C engines and underwing hard-points; and the AP.68TP-600 Viator, which is similar to the Spartacus but has a lengthened fuselage and a retractable undercarriage. The AP-68TP being jointly developed with Aeritalia.

Taneja Aerospace & Aviation Ltd in India undertook to set up a project for manufacture of P-68 aircrafts with three variants: P-68C (twin piston engine, non pressurised), P-68 C-TC (twin piston engine turbo Charged) and P-68 Observer (same as P-68 C-TC with forward and downward view equal to that of a helicopter). It has an empty weight of 1320 Kgs and payload of 764 Kgs, with a capacity to attain a maximum speed of 322 Kmph, 1550 ft./min rate of climb, landing run of 215 mtrs and an optimum cruising range of 2170 Kms at 12000 ft.

The aircraft was manufactured by Taneja Aerospace in India, while Aerocosmos, which held the production rights, was purchased by Air Samanta in 1998.

Vulcanair S.P.A of Naples, Italy, were manufacturers of Partenavia P68 aircraft in 2004. Vulcanair was converting one of its P68 Observer airframes to diesel power with an SMA engine. This was due to fly in September 2003 and if successful will be offered onto the light twin market.

More than 500 P68s had been built to 2003, of which some 35 are of the Observer vari¬ant for law enforcement and paramilitary use.

Gallery

P-68B Observer
Engines two 200-hp (149-kW) Lycoming IO- 360-A1B6
Wing span 39 ft 4.5 in / 12.00 m
Length 30 ft 8 in / 9.35 m
Height 11 ft 1.75 in / 3.40 m
Wing area 200.2 sq ft / 18.60 sq.m
Gross wt. 4,321 lb / 1,960 kg
Empty wt. 2,822 lb / 1,280 kg
Max Speed 174 kts / 200 mph / 322 km/h at sea level
Max Cruise 165 kts
Initial climb rate 1,160 / 488 m fpm
Range 920 nm / 1,358 miles / 2,186 km
Service ceiling 20,000 ft / 6,095 m
Armament: none
Seats 7

P.68 Observer 2

P-68C
Engines: 2 x 200 hp Lycoming IO-360-A1B6
Seats: 6/7
Empty Wt: 2787 lbs
Gross wt: 4387 lbs
Useful load: 1600 lbs
Max Cruise: 175 mph
Max range: 900 sm

P-68TC
Engines two 210-hp turbocharged Lycoming IO-360C-1A6D
Gross wt. 4,387 lb
Empty wt. 2,866 lb
Fuel capacity 137-196 USG
Max Speed 190 kts
Max Cruise 175 kts
Initial climb rate 1,130 fpm
Range 1,040 nm
Ceiling 27,000 ft
Seats 7

AP-68TP
Engines: 2 x 240 hp Allison 250
Seats: 7/8
Empty Wt: 3415 lbs
Gross wt: 5787 lbs
Useful load: 2372 lbs
Max Cruise: 240 mph
Max range: 820 sm

AP 68 TP 600 Viator
Engines: 2 x Allison 250 B17C, 222 shp
Length: 35.761 ft / 10.9 m
Height: 11.811 ft / 3.6 m
Wingspan: 39.37 ft / 12.0 m
Wing area: 200.21 sq.ft / 18.6 sq.m
Max take off weight: 6284.3 lb / 2850.0 kg
Weight empty: 3616.2 lb / 1640.0 kg
Max. weight carried: 2668.1 lb / 1210.0 kg
Max. speed: 220 kts / 408 km/h
Landing speed: 70 kts / 130 km/h
Cruising speed: 170 kts / 315 km/h
Initial climb rate: 1929.13 ft/min / 9.8 m/s
Service ceiling: 25000 ft / 7620 m
Wing loading: 31.37 lb/sq.ft / 153.0 kg/sq.m
Range: 445 nm / 824 km
Crew: 2
Payload: 9-12pax

Parseval PL-14 / Puffin / Burevestnik / Petrel / Parseval II

Built in 1913 by Luft-Fahrzeug-Gesellschaft, the non-rigid Parseval PL-14 Burewestnik was purchased in Germany by the Russian Federation and called “Parseval-II” (maybe was called “Puffin” or “Burevestnik / Petrel”).

Burevestnik was filled with gas in the first half of November, 1914 and executed some flights before it was recognized as unsuitable in fighting conditions. It was armed with machine guns and had bombs. It was not used in combat. It flew with the Russian Federation until disassembled in Spring 1915.

Engines: 2 x 177 h.p
Envelope volume: 9600 cu.m
Length: 86 m
Width: 16 m
Maximum speed: 67 kph
Endurance: 20 hr

ParaPlane Corp Paraplane

Single seat twin engined motorised parachute with constant chord. Control inputs through pedals for yaw. Pilot suspended below wing in trike unit. Undercarriage has three wheels in tricycle formation. Nosewheel steering. No brakes. Aluminium tube trike unit, without pod. Engines mounted below wing driving pusher propellers.
The ParaPlane, which is listed as an ultralight in the USA, is in fact a motorised parachute. Shown at Sun ‘n’ Fun in March 1983 at Lakeland, Florida, this amazing flying machine only flew once due to difficult weather conditions.

Designed by Steve Snyder, the ParaPlane uses as its ‘wing’ a 28.5 ft (8.69 m) parachute of constant chord giving 375 sq.ft (34.8 sq.m) of lifting surface. For pilots heavier than 185 lb (84kg), it can also be equipped with a 36.0ft ‘wing’ of 450sq.ft (10.97 m, 41.8 sq.m). The contraption is flown like a non powered parachute wing, its pilot steering via lines attached to foot pedals to give directional control. The rear wheels of the trike unit are free to castor and are unbraked, the structure being made of alumi-nium tubes with a hammock seat and shoulder harness. Behind the seat, the engine mount carries the two Solo 210cc 15hp engines driving two twin blade contra rotating prop¬ellers.

Weighing 79 lb (36 kg) empty, the trike unit is foldable down to 50 x 14 x 20 inch (127 x 35 x 51 cm). The aircraft is used like an ascending parachute and it collapses behind the trike unit when it lands. Take off is made at 25 mph (40 kph), which is also the landing speed. ParaPlane Corporation does not quote a stalling speed, though a figure of 8 10mph (13 16kph) is mentioned.

Price: from $3750 in 1983.

During the 1983 Oshkosh ParaPlane rook over 1000 orders for the craft.

Engine: 2 x Solo 215 (2 x 215cc) 33hp
Empty wt: 163 lbs
Wing span: 30’6”
Wing area: 400 sq.ft
Fuel cap; 4.5 USG
Construction: Aluminium, Nylon
Max wt: 360 lbs
Max speed: 26 mph
Climb rate: 250 fpm
Design limit: +9g
Glide ratio: 3-1
Wing loading: 0.9 lbs/sq.ft
Power loading: 11.0 lbs/hp

Engine: 2 x Solo 335, 15 hp each
Propeller diameter 50 inch, 1.27 m
Belt reduction
Power per unit area 0.08 hp/sq.ft, 0.86 hp/ sq.m
Fuel capacity 4.5 US gal, 3.8 Imp gal, 17.0 litre
Length overall 5.7ft, 1.73m
Height overall 5.6ft, 1.70m
Wing span 28.5ft, 8.69 m
Constant chord 13.0 ft, 3.96 m
Total wing area 375 sq.ft, 34.8 sq.m
Empty weight 140 lb, 64 kg
Max take off weight 355 lb, 161 kg
Payload 215 lb, 98 kg
Max wing loading 0.95 lb/sq.ft, 4.6 kg/sq.m
Max pow¬er loading 11.8 lb/hp, 5.4 kg/hp
Max level speed 30 mph, 48 kph
Never exceed speed 30 mph, 48 kph
Max cruising speed 30 mph, 48 kph
Economic cruising speed 25 mph, 40 kph
Best glide ratio with power off 3/1
Range at average cruising speed 41 mile, 66 km

Panavia MRCA / Tornado

Tornado

The requirement for a new multi-role combat aircraft (MRCA) to equip the German Luftwaffe and Marineflieger, Italy’s Aeronautica Militare and the UK’s RAF was established in the mid-1960s. This led, on 26 March 1969, to formation of the European industrial company Panavia Aircraft GmbH, combining the aviation talents of Aeritalia, British Aerospace and Messerschmitt-Bölkow-Blohm to design, develop and manufacture this important aircraft. The feasibility study for an aircraft to meet the tri-national requirements was completed by 1 May 1969, and within four years a go-ahead for the Panavia MRCA was given; between then and the flight of the first prototype (D-9591), flown at Manching, Germany on 14 August 1974, piloted by the project test pilots, Paul Millett with Nils Meister in the second seat. This is the first of nine prototypes and six pre-series aircraft to fly. Two more prototypes were to fly at Warton, one at Manching and one at Caselle.

Panavia Tornado Article

The initial production agreements for the Tornado envisage a total of 809 aircraft and comprise 644 of the (IDS) interdictor/strike version for the Aeronautica Militare (100), Luftwaffe (212), Marineflieger (112), and RAF (220), plus an additional 165 examples for the RAF of the air-defence variant (ADV, first flown in October 1979).

The aircraft has variable geometry wings and is powered by two Turbo-Union RB199-34R turbofans, with a maximum speed of 1452 mph and a service ceiling of 50000 feet. The Air Defence Variant (ADV) version of the Tornado is optimised for long-range interception with radar and infra-red guided air-to-air missiles and one internally mounted 27mm Mauser cannon.

Compared to the initial IDS variant, the Tornado ADV has a longer fuselage with additional fuel capacity, a better fineness ratio for enhanced transonic acceleration, and the possibility of locating four Sky Flash air-to-air missiles in semi-recessed positions in the lower fuselage.

Tornado ADV

The air defense variant (ADV) of Tornado, developed specifically for the RAF as a long-range air defense interceptor has GEC-Marconi Foxhunter multimode radar in place of the IDS’s ground-mapping radar and terrain-following radar, although some 80 percent commonality was achieved between the types.

The first production IDS versions were flown, chronologically, by the UK (10 July 1979), West Germany (27 July 1979) and Italy (25 September 1981), early production aircraft going to the Trinational Tornado Training Establishment (opened in 1981) which was set up at RAF Cottesmore and which, by August 1982, had received its full complement of 50 aircraft. The RAF also has a Tornado Weapons Conversion Unit (TWCU) at RAF Honington, the other three services each conducting their own weapons conversion training with national avionics and weapons.

The first of 229 Tornado GR.1 strike aircraft was delivered to the Royal Air Force in 1981 and the first squadron equipped with the aircraft became operational in 1982. The GR.1 is capable of carrying a wide range of armaments, including conventional and anti-airfield bombs, laser-guided bombs, air-to-ground rockets and anti-radar missiles.

Early tests carried out in 1980 showed that the aircraft’s weapon system was capable of highly accurate bomb delivery, and this has been confirmed more recently by Tornados competing for the first time in the USAF’s 1984 ‘Giant Voice’ bombing competition held in South Dakota. Tornado GR.Mk1s of No. 617 (Dambuster) Squadron, competing against Boeing B-52s and General Dynamics FB-111As of Strategic and Tactical Air Commands, and RAAF F-111Cs, took first and second place in the LeMay Trophy contest (high-and low level sorties) first and third places in the John C. Meyer Trophy contest (for the best non-B-52 crew in low-level attack) and second and sixth place in the Mathis Trophy contest (for the best high and low-level team bombing scores). This is the first time that teams from outside the US have won the LeMay or John C. Meyer trophies, and such capability augurs well for the Tornado and NATO.

Features of the design include a variable geometry wing, sweeping from 25′ to 68′, two RB199 three-shaft turbofans developed by Turbo-Union, (which combines Fiat Aviazione, MTU München and Rolls-Royce) and, because of the trinational requirement, some variations in avionics and communications equipment.

This advanced equipment provides each nation with an aircraft having day and night all weather extremely low-level interdictor/ strike capability, the RAF designating this version Tornado GR.Mk1.

The first prototype of the RAF’s ADV variant, designated Tornado F.Mk2, was flown first on 27 October 1979, and this differs structurally in having the overall length being increased by 4 ft 5.5 in (1.36 m) to permit tandem carriage of AAMs, and the fixed portion of the wings being extended forward, increasing chord. Increased internal fuel capacity, plus drop tanks on the inner underwing stations, allowed one of the prototypes to demonstrate a 2 hours 20 minutes combat air patrol (CAP) on station 374 miles (602 km) from base, but a nose-mounted (port) retractable inflight-refuelling probe will allow more extended CAPs. Armament of this version comprises a 27-mm IWKA-Mauser cannon in the fuselage, plus two AIM-9L Sidewinder (underwing) and four Sky Flash (underfuselage) air-to-air missiles. The first two Tornado F.Mk2s for RAF service were handed over to the F-2 Operational Conversion Unit at RAF Coningsby, Lincolnshire in early November 1984.

Tornado F2A

Apart from dual controls and minor differences in the navigator’s equipment, the trainer Tornadoes are identical to the strike aircraft and possess full operational capability.

A total of 929 Tornados has been ordered in seven batches for the air arms of the three partner countries and two export custom¬ers. In addition, four development aircraft will be reworked to production standard. Production in Italy was completed by 1987, but continues at a rate of 44 per year in the UK and 42 per year in Germany. By mid-1987 620 aircraft had been delivered. Two basic versions are in production:

IDS The sixth batch of aircraft already incorporates some avionic upgrades, including the MIL standard 1553B digital databus, uprated mission computers, and missile control systems associated with the integration of Alarm (for the RAF) and AGM-fl 85 Harm (for West Germany). The Luftwaffe selected the electronic, combat, and reconnaissance (ECR) variant of the IDS Tornado in 1986, and placed an order for 35 aircraft. Optimised for the stand-of reconnaissance and anti-radiation roles, the ECR will feature an emitter locator system, a datalink, a low/medium altitude recon¬naissance system, and jammer pods. Normal weapons load will comprise two Harms and two Sidewinder AAMs, with ECM/flare dispenser and external fuel tanks. The twin Mauser 27mm guns are omitted.

ADV The first prototype of the Tornado Air Defence Variant, A01 s/n ZA254, com¬pleted more than 41 hr flying by the end of January 1980 when it went on lay up for the installation of updated equipment. The aircraft made its first flight on 27 October 1979. Early ADVs were fitted with RB.199 Mk.1OU engines and designated F.2s, while the 1987 production model is the F.3 with Mk.104 engines and other equipment upgrades. F.2s will be retrofitted to F.3 standard except for the engine change, and will be known as F.2As. Designed specifically to meet RAF require¬ments for a long-range all-weather interceptor, the Tornado ADV features an advanced track-while-scan pulse-Doppler radar, twin inertial platforms, an updated main computer, advanced displays, and (on the F.3) automatic wing sweep and the automatic manoeuvre device system which controls flap/slat scheduling. Initial armament consists of mixed of Skyflash and Sidewinder AAMs.

The RAF’s first Tornado fighter squadron, No. 29, was equipped with Tornado F.3s, the definitive version powered by RB.199 Mk.104s and carrying four Sidewinders (instead of two as on the F.2) plus four Sky Flash missiles.

The 1990 cancellation of 33 Tornados for the RAF meant that production was likely to end in 1992. To 1990, more than 900 Tornados had been ordered for the air arms of the three partner countries and Saudi Arabia, with other export orders in abeyance. As well as operating the IDS attack version, the Luftwaffe is receiving 35 electronic, combat and reconnaissance (ECR) variants. Four Skyflash AAMs, Sidewinders and a 27mm cannon armament.

The ECR (electronic combat and reconnaissance) version was a Tornado variant developed by the Germans for the reconnaissance role and suppression of enemy air defense with the AGM-88A HARM anti-radar missile.

Tornado ECR

The first production Tornado ECR flew on 26 October 1989.

44+00 JBG-31, 28 Aug 1988

The RAF received 170 ADVs, of which 152 were in F.Mk 3 improved form. Saudi Arabia was the only other customer, having 24.

GR.1 is the RAF designation for the RAF Tornado IDS aircraft. The GR.1A was a modified variant optimized for the recconnaisance role and the GR.1B for the maritime attack role equipped with Sea Eagle missiles.
Intended as a mid-life update of the Tornado GR.1 fleet, deliveries of the Tornado GR.4 began in October 1997. All GR.1 and GR.1B aircraft that remained in service were upgraded to GR.4 standard. All GR.1A have been upgraded to GR.4A, the reconnaissance version of the GR.4. The GR.4/4A update enables the RAF Tornado IDS aircraft to remain in service for at least another 10-15 years. While the performance of the aircraft is similar, overall effectiveness is enhanced by a forward–looking infra-red system, a wide-angle head-up display, night vision goggles, new defensive systems and avionics and provision for enhanced anti-armour, stand-off attack and laser designation weapons.

A ceremony was held at Warton on June 10, 2003 to celebrate the hand over by BAE Systems of the 142nd and last Tornado GR.4 to the RAF. Over £1bn has been spent on this Mid Life Update which began with contract signature back in July 1994. The first air¬craft was delivered on October 31, 1997, though since then the time needed to do the work on each aircraft has been reduced by 40%. One of the aims of the modification of the GR.1 and GR.1A into the GR.4 and GR.4A respectively has been to give the RAF a common fleet standard. The aircraft is now able to carry more smart weapons such as the Storm Shadow cruise missile as well as use the RAPTOR reconnaissance pod. Other major improvements include a Forward Looking Infra Red (FLIR) sensor, new Head Up Display (HUD), NVG compatible cockpit, GPS navigation, provision for a TIALD pod and new electronic warfare system.

Tornado GR.4

Until delivery of the final aircraft was in 1998, orders covered 781 production IDS Tornadoes for interdictor strike and ECRs for electronic combat and reconnaissance, as 228 IDSs for the RAF, 210 IDS and 35 ECR for the Luftwaffe, 112 IDSs for the German Navy, 99 IDSs for the Italian Air Force, and 96 IDSs for Saudi Arabia.

During the 1991 Gulf War, the Tornado GR.1 force flew 1500 operational sorties mainly against airfields, air defence sites and bridges. Six aircraft were lost in low-level missions.

Germany’s Mid Life Update (MLU) for the Tornado was completed. And also the Italian Air Force (AMI) Tornado IDS and ECR were scheduled to receive a mid life update. AMI Tornado F.3s that were leased from the RAF were returned to the UK, and were to be replaced by leased F-16s until the arrival of the Eurofighter Typhoon.

The UK’s Ministry of Defence was pioneering an approach to building its next-generation Tempest fighter—by recycling retired Tornado jets. Instead of sourcing expensive foreign materials, old fighter jet parts are ground into a titanium-rich powder used for 3D printing new aircraft components.
Rolls-Royce has successfully tested these parts in an Orpheus engine, proving their viability. This initiative not only reduces costs but also strengthens supply chain resilience. With Italy and Japan also involved, the Tempest program is set to revolutionize sustainable aircraft manufacturing, with a planned first flight in 2026 and entry into service by 2035.
While this approach might sound crazy, it actually reduces the country’s reliance on foreign-sourced materials and points toward some incredible new ways to recycle old aircraft.
Introduced as a response to lingering concerns about how the global market for vital materials could be impacted by large-scale war between great powers, this is an area of increasing focus for the Future Combat Air Systems (FCAS) program. The FCAS is Britain’s overarching effort that includes the development of the crewed Tempest fighter.
“Through the expected lifecycle of the U.K.’s FCAS, we expect access to critical materials to be challenged, as global supply chains become increasingly disrupted and competitive. In parallel, there is a societal need to make the best use of the raw materials we already have,” explained the Future Combat Air System’s Sustainability Requirements Manager, identified only as “Squadron Leader Rob.”
To achieve this, rather than just scrapping old Tornado GR4s that were retired from active service in 2019 and then sourcing all the high-quality raw materials needed for the new Tempest fighter program from foreign countries, the U.K. will simply yank parts off of those old Tornados and feed them into an industrial grinder to produce a powder, called “feedstock.” This powder can then be used by industrial 3D printers to produce new components for new fighters.
The British Ministry of Defense, is collaborating with Rolls Royce in the effort.
In testing so far, Tornado engine compressor blades, which include a high quantity of titanium, were cleaned, ground up, and then used to 3D print a new nosecone and compressor blades for “Orpheus” the small engine Rolls Royce has in testing to mature technologies for the Tempest program.
With its new 3D-printed component, the Orpheus engine was then put through the wringer and managed to pass all suitability and safety tests.

“Tornado 2 Tempest is a bold, exciting and innovative project and a demonstration of how excellent collaboration between the MOD, industry and SME can deliver sustainable and technologically advanced solutions,” said Andrew Eady, Rolls-Royce Vice President for FCAS Sustainability.
This same recycling and 3D-printing process can be used for steel and aluminum components as well, which would further reduce waste, and allow the U.K. to have to mine and process fewer raw materials in the future.
“Not only can this solution reduce the costs and burden of sourcing critical and high-value metals, but it can also produce components that are lighter, strong and longer lasting than those made through traditional forging techniques, thereby further enhancing the MOD’s overall sustainability and effectiveness,” Thomas Powell, DRDT’s Strategic & Submarine Recycling Senior Commercial Manager, said in a Rolls Royce press release.
Construction of the first Tempest technology demonstrator began 2024, and the U.K., Italy, and Japan, which are also partner countries in the program, are hoping to see the aircraft make its first test flight in 2026, with the goal of getting these fighters into service by 2035.

Gallery

Tornado ADV
Engines: 2 x Turbo-Union RB.199
Installed thrust (dry / reheat): 80 / 142+ kN
Span: 13.9 m / 8.6 m
Length: 18.1 m
Wing area: approx. 25 sq.m
Empty wt: 14,500 kg
MTOW: 27,968 kg
Warload: 8,500 kg
Max speed: 2.2 Mach
Time to height: 2 min / 9150 m
Ceiling: 21,300+ m
TO run: 760 m
Ldg run: 370 m
Fuel approx. internal (external): 7300 lt (6000 lt)
Air refuel: Yes
Combat radius: 740+ km
Armament: 8 x AAM, 1 x 27 mm

Tornado IDS
Powerplant: two Turbo-Union RB.199-34R Mk.101 turbofans, 37.70kN (8,475lbst) dry and 66.01kN (14,840lbst) with afterburning
Length 16.72m (54ft 10.25in)
Height 5.95m (19ft 6.25in)
Wingspan at minimum sweep (25 deg) 13.91m (45ft 7.5in)
Wingspan at maximum sweep (67 deg) 8.60m (28ft 2.5in)
Take-off (’empty’) 14091kg (31,065lb)
Max Take-Off Weight 27961kg (61,620lb)
Max level speed ‘clean’ at 11000m (36,090ft) Mach 2.2+/ 2337+km/h /1453+mph)
Service ceiling 50,000+ ft (15420+ m)
Armament: two internal Mauser BK.27 27mm cannons / 180 rounds each
Hardpoints: 9
External load: 18,000 lb / 8165 kg
Max range: 3885 km
Air refuel: Yes
Combat radius hi-lo-hi: 1400 km
Crew: 2

Tornado IDS
Powerplant: two Turbo-Union RB.199-34R Mk.103 turbofans each rated at 38.48kN (8,650lbst) dry and 71.50kN (16,075lbst) with afterburning
Length 16.72m (54ft 10.25in)
Height 5.95m (19ft 6.25in)
Wingspan at minimum sweep (25 deg) 13.91m (45ft 7.5in)
Wingspan at maximum sweep (67 deg) 8.60m (28ft 2.5in)
Take-off (’empty’) 14091kg (31,065lb)
Max Take-Off Weight 27961kg (61,620lb)
Max level speed ‘clean’ at 11000m (36,090ft) Mach 2.2+/ 2337+km/h /1453+mph)
Service ceiling 50,000+ ft (15420+ m)
Armament: two internal Mauser BK.27 27mm cannons / 180 rounds each
Hardpoints: 9
Max range: 3885 km
Air refuel: Yes
Combat radius hi-lo-hi: 1400 km
Crew: 2

Tornado F.2
Seats: 2
Wing span: 45 ft 8 in (13.9m)

Tornado F.3
Engines: 2 x 16,910 lb st (71,2 kN) Turbo-Union RB199 Mk103 turbofans
Seats: 2
Wing span: 45 ft 8 in (13.9m)

Tornado GR.1
Seats: 2
Wing span: 45 ft 8 in (13.9m)

Tornado GR.4

PAM 100B

PAM 100B Single place, stand-on Individual Lifting Vehicle (ILV) with two composite 24″ diameter props for directional control. Simple tubular helicopter-type high strength airframe made of aircraft grade aluminum. Controls consist of a throttle and a fly-by-wire joy stick for directional control. There is no collective control. Kit price of $50,500 includes everything but shipping in 2009. Plans were also available.

Engines: (2) Hirth F-30 100 hp
Rotor Blades: Four extruded aluminum
Blade diameter: 9.17 ft
Chord: 8″ chord

Min Speed Hover
Cruise 45 mph
Top Speed 60 mph
Empty Weight 640 lbs
Useful Load 360 lbs
Gross Weight 1,000 lbs
Skid Width 10 ft
Height 9 ft
Length 8 ft

Palmgren American

A monoplane equipped with two 50-horse power motors and two propellers. There are two blades in front and three in the rear. Built of steel tubing and aluminium, the machine weighed 1,000 pounds and had a stated carrying capacity of twelve persons. Designed and built by David A. Palmgren, as displayed at the Grand Central Palace Aero Exhibition, New York, in May 1912.