JEROEN VOGELAAR: Aviation Photographs

Jeroen Vogelaar

Focke-Wulf A 16

Focke-Wulf A.16 D437 Bremen

The Focke-Wulf A.16 was a German three/four passenger light transport monoplane.

  • Role: Light passenger transport
  • National origin: Germany
  • Manufacturer: Focke-Wulf Flugzeugbau AG
  • Designed by: Heinrich Focke and Georg Wulf
  • First flight: 1924
  • Number built: 20+

Focke-Wulf A.16 D437 Bremen

Specifications (A.16c)

General characteristics

  • Crew: 1
  • Capacity: 3–4
  • Length: 8.5 m (27 ft 1034 in)
  • Wingspan: 13.90 m (45 ft 714 in)
  • Height: 2.30 m (7 ft 612 in)
  • Wing area: 27.1 m2 (291 ft2)
  • Empty weight: 570 kg (1256 lb)
  • Gross weight: 970 kg (2138 lb)
  • Powerplant: 1 × Siemens-Halske Sh 11 7-cylinder radial piston engine, 56 kW (75 hp)

Performance

  • Maximum speed: 135 km/h (84 mph)
  • Range: 550 km (342 miles)
  • Service ceiling: 2500 m (8200 ft)

Gulfstream G550

Gulfstream G550 N917GA

Gulfstream G550 is a business jet aircraft. The Gulfstream 550 has the longest flight range in its class.

 

  • Role: Business jet
  • National origin: United States of America
  • Manufacturer: Gulfstream Aerospace
  • Production line: Savannah, Georgia
  • First flight: July 18, 2002
  • Introduction: 2004
  • Status: In service
  • Produced: 2003–present
  • Number built: 300+

Specifications G550

General characteristics

  • Crew: 2 pilots, 0–2 attendants
  • Capacity: 14–19 passengers
  • Length: 96 ft 5 in (29.4 m)
  • Wingspan: 93 ft 6 in (28.5 m)
  • Height: 25 ft 10 in (7.9 m)
  • Empty weight: 48,300 lb (21,900 kg)
  • Loaded weight: 54,500 lb (24,700 kg)
  • Useful load: 6,200 lb (2,800 kg)
  • Max. takeoff weight: 91,000 lb (41,300 kg)
  • Powerplant: 2 × Rolls-Royce BR710 turbofan, 15,385 lbf (68.44 kN) each
  • Maximum Ramp Weight: 91,400 lb (41,500 kg)
  • Maximum landing weight: 75,300 lb (34,200 kg)
  • Maximum fuel weight: 41,300 lb (18,700 kg)
  • Cabin dimensions: volume: 1,669 ft³ (47.3 m³), height: 6 ft 2 in (1.88 m), width: 7 ft 4 in (2.24 m)
  • Baggage compartment volume: 226 ft³ (6.4 m³)

Performance

  • Maximum speed: 0.885 Mach (585 mph, 941 km/h)
  • Cruise speed: 488 knots (562 mph, 0.85 Mach, 904 km/h)
  • Range: 6,750 nmi (7,768 miles, 12,500 km)
  • Service ceiling: 51,000 ft (15,500 m)
  • Takeoff distance: 5,910 ft (1,800 m)
  • Landing distance: 2,770 ft (880 m)

 

Boeing 787 Dreamliner

Boeing 787-8 PH-TFL ArkeFly

The Boeing 787 Dreamliner is a long-range, mid-size wide-body, twin-engine jet airliner developed by Boeing Commercial Airplanes.

 

  • Role: Wide-body jet airliner
  • National origin: United States
  • Manufacturer: Boeing Commercial Airplanes
  • First flight: December 15, 2009
  • Introduction: October 26, 2011, with All Nippon Airways
  • Status: In service
  • Produced: 2007–present
  • Number built: 269 as of April 2015

Specifications

General characteristics

Boeing 787-8

First Flight: December 15, 2009

  • Cockpit crew: 2
  • Seating capacity: 381 (maximum)
  • Overall length: 186 ft 1 in (56.7 m)
  • Wingspan: 197 ft 3 in (60.1 m)
  • Overall height: 55 ft 6 in (16.9 m)
  • Fuselage width: 18 ft 11 in (5.77 m
  • Fuselage Height: 19 ft 7 in (5.97 m)
  • Operating empty weight: 259,500 lb (118,000 kg)
  • Maximum landing weight: 380,000 lb (172,000 kg)
  • Maximum take-off weight: 502,500 lb (228,000 kg)
  • Service ceiling: 43,000 ft (13,100 m)
  • Cruising speed: Mach 0.85 (567 mph, 490 knots, 913 km/h at 35,000 ft/10,700 m)
  • Maximum speed: Mach 0.90 (593 mph, 515 knots, 954 km/h at 35,000 ft/10,700 m)
  • Range fully loaded: 7,850 nmi (14,500 km; 9,030 mi)
  • Engine (× 2): General Electric GEnx-1B or Rolls-Royce Trent 1000 thrust: 64,000 lbf (280 kN)

Boeing 787-9

Boeing 787-9 Dreamliner PH-BHD KLM

Boeing 787-9 Dreamliner PH-BHD KLM

First Flight: September 17, 2013

  • Cockpit crew: 2
  • Seating capacity: 420 (maximum certificated)
  • Overall length: 206 ft 1 in (62.8 m)
  • Wingspan: 197 ft 3 in (60.1 m)
  • Overall height: 55 ft 10 in (17.0 m)
  • Fuselage width: 18 ft 11 in (5.77 m
  • Fuselage Height: 19 ft 7 in (5.97 m)
  • Operating empty weight: 304,000 lb (138,000 kg)
  • Maximum landing weight: 425,000 lb (193,000 kg)
  • Maximum take-off weight: 557,000 lb (253,000 kg)
  • Service ceiling: 43,000 ft (13,100 m)
  • Cruising speed: Mach 0.85 (567 mph, 490 knots, 913 km/h at 35,000 ft/10,700 m)
  • Maximum speed: Mach 0.90 (593 mph, 515 knots, 954 km/h at 35,000 ft/10,700 m)
  • Range fully loaded: 8,300 nmi (15,400 km; 9,550 mi)
  • Engine (× 2): General Electric GEnx-1B or Rolls-Royce Trent 1000 thrust: 71,000 lbf (320 kN)

Boeing 787-10

First Flight:

  • Cockpit crew: 2
  • Seating capacity: 323 (3-class) (maximum certificated)
  • Overall length: 224 ft 1 in (68.3 m)
  • Wingspan: 197 ft 3 in (60.1 m)
  • Overall height: 55 ft 10 in (17.0 m)
  • Fuselage width: 18 ft 11 in (5.77 m
  • Fuselage Height: 19 ft 7 in (5.97 m)
  • Operating empty weight: 304,000 lb (138,000 kg)
  • Maximum landing weight: 445,000 lb (202,000 kg)
  • Maximum take-off weight: 557,000 lb (253,000 kg)
  • Service ceiling: 43,000 ft (13,100 m)
  • Cruising speed: Mach 0.85 (567 mph, 490 knots, 913 km/h at 35,000 ft/10,700 m)
  • Maximum speed: Mach 0.90 (593 mph, 515 knots, 954 km/h at 35,000 ft/10,700 m)
  • Range fully loaded: 7,020 nmi (13,000 km; 8,080 mi)
  • Engine (× 2): General Electric GEnx-1B or Rolls-Royce Trent 1000 thrust: 76,000 lbf (340 kN)

Arado Ar 96

Arado Ar 96 B-1 U-CF Luftwaffe

The Arado Ar 96 was a German single-engine, low-wing monoplane of all-metal construction military trainer produced by Arado Flugzeugwerke.

  • Role: Military Trainer
  • National origin: Germany
  • Manufacturer: Arado Flugzeugwerke
  • First flight: 1938
  • Introduction: 1939
  • Status: 2 aircraft in museums
  • Number built: ca 3,500

Operators

  • Bulgarian Air Force
  • Czechoslovakian Air Force
  • French Air Force (Postwar)
  • Luftwaffe
  • Hungarian Air Force
  • Romanian Air Force
  • Slovenské vzdušné zbrane

Arado Ar 96 B-1 U-CF Luftwaffe

Survivors

Specifications (Arado Ar 96B-2)

General characteristics

  • Crew: 2
  • Length: 9.1 m (29 ft 10 in)
Ar 396A-1: 9.3 m (31 ft)
  • Wingspan: 11 m (36 ft 1 in)
  • Height: 2.6 m (8 ft 6 in)
Ar 396A-1: 2.45 m (8 ft)
  • Wing area: 17.1 m2 (184 sq ft)
Ar 396A-1: 18.3 m2 (197 sq ft)
  • Empty weight: 1,295 kg (2,855 lb)
Ar 396A-1: 1,643 kg (3,622 lb)
  • Max takeoff weight: 1,700 kg (3,748 lb)
Ar 396A-1: 2,060 kg (4,542 lb)
  • Powerplant: 1 × Argus As 410A-1 inverted V-12 air-cooled piston engine, 347 kW (465 hp)
Ar 396A-1: 1 x 433 kW (581 hp) Argus As 411MA inverted V-12 air-cooled piston engine
  • Propellers: 2-bladed variable pitch metal propeller

Performance

  • Maximum speed: 330 km/h (205 mph; 178 kn) at sea level
  • Cruising speed: 295 km/h (183 mph; 159 kn)
Ar 396A-1: 275 km/h (171 mph) at sea level
  • Range: 990 km (615 mi; 535 nmi)
Ar 396A-1: 600 km (373 mi)
  • Service ceiling: 7,100 m (23,294 ft)
Ar 396A-1: 6,900 m (22,638 ft)
  • Rate of climb: 5.083 m/s (1,000.6 ft/min)
  • Time to altitude:
Ar 396A-1: 4,000 m (13,123 ft) in 10 minutes 18 seconds
Armament

1 × 7.92 mm (0.312 in) MG 17 machine gun

Ar 396A-1: 1 × 7.92 mm (0.312 in) MG 17 machine gun + 2 x 50 kg (110 lb) bombs on underwing racks

Heinkel He 162

Heinkel He162A-2 Volksjäger 120076/4 Luftwaffe

The Heinkel He 162 Volksjäger, the name of a project of the Emergency Fighter Program design competition, was a German single-engine, jet-powered fighter aircraft fielded by the Luftwaffe in World War II. Designed and built quickly, and made primarily of wood.

  • Role: Fighter
  • National origin: Germany
  • Manufacturer: Heinkel
  • First flight: 6 December 1944
  • Introduction: 1945
  • Status: 9 aircraft in museums
  • Retired: 1945
  • Number built: ca 320

Specifications (He 162A)

General characteristics

  • Crew: 1, pilot with ejection seat
  • Length: 9.05 m (29 ft 8 in)
  • Wingspan: 7.2 m (23 ft 7 in)
  • Height: 2.6 m (8 ft 6 in)
  • Wing area: 11.16 m² (156 ft²)
  • Empty weight: 1,660 kg (3,660 lb)
  • Max. takeoff weight: 2,800 kg (6,180 lb)
  • Powerplant: 1 × BMW 003E-1 or E-2 (meant for dorsal fuselage attachment) axial flow turbojet, 7.85 kN (1,760 lbf)
  • Fuel capacity of 695 litres (183 US gallons), allowing maximum 30 minute mission profile

Performance

  • Maximum speed: 790 km/h (491 mph) at normal thrust at sea level; 840 km/h (522 mph) at 6000 m (19,680 ft); using short burst extra thrust 890 km/h (553 mph) at sea level and 905 km/h (562 mph) at 6000 m (19,680 ft).
  • Range: 975 km (606 mi)
  • Service ceiling: 12,000 m (39,400 ft)
  • Rate of climb: 1,405 m/min (4,615 ft/min)

Armament

  • Guns: 2 × 20 mm MG 151/20 autocannons with 120 rpg (He 162 A-2) OR 2 × 30 mm MK 108 cannons with 50 rpg (He 162 A-0, A-1)

Deutsches Technikmuseum Berlin

Heinkel He162A-2 Volksjäger 120076/4 Luftwaffe

The Deutsches Technikmuseum Berlin has more than 40 aircraft and large-scale objects on display including: Arado Ar96B, Heinkel He162A-2 Volksjäger, Junkers Ju87R-4, Messerschmitt Bf109E-3, Messerschmitt Bf110F-2, Junkers Ju88G-1 and many more.

Deutsches Technikmuseum Berlin
Trebbiner Str. 9
10963 Berlin-Kreuzberg
Germany

 

D-EMVT

U-CF

A-43

RM+HE

45-0951

D-ENTE

D437

D-IBAO

TV+UB

120076/4

A180/14

257

803/17

CF-ALX

D-AZAW

L1+BL

F-PCDA

D-EDOD

1323

257

1407/+5

5052/LN+NR

MM541256

331/PN

N614GB

Arado Ar79

Arado Ar96B

Bucker Bu131B Jungmann

Bucker Bu181C-2 Bestmann

Douglas C-47B Skytrain

Fiesler S14 (Fi156C-3) Storch

Focke-Wulf A-16

Focke Wulf Fw44 Stieglitz

Fokker D.VII

Gotha Go242A

Halberstadt CL.IV

Halberstadt CLS.1

Heinkel He162

Heinkel He162A-2 Volksjäger

Henschel Hs126B-1

Jeannin Stahltaube

Junkers J1

Junkers F-13 G1E

Junkers Ju52/3m

Junkers Ju87R-4

Klem L-25b

Klem Sk15A (K135D)

Lim-5

Messerschmitt N1002 (BF108)

Messerschmitt Bf109E-3

Messerschmitt Bf110F-2

North American F-86K Sabre

SNCAN N1101 Noralpha

SNCAC NC702 Martinet

VFW 614

 

 

Antonov An-12

Antonov An-12AP UR-CCP Cavok Air

The Antonov An-12 is a four-engined turboprop transport aircraft designed in the Soviet Union.

  • Role: Civil and Military transport aircraft
  • National origin: Soviet Union
  • Manufacturer: Antonov
  • First flight: 16 December 1957
  • Introduction: 1959
  • Status: Active service with various airlines (especially cargo) and Air Forces
  • Produced: 1957–1973
  • Number built: 1,248

Specifications (An-12)

General characteristics

  • Crew: 5: 2 pilots, flight engineer, navigator, radio operator
  • Payload: 20,000 kg (44,000 lb)
  • Length: 33.10 m (108 ft 7 in)
  • Wingspan: 38.00 m (124 ft 8 in)
  • Height: 10.53 m (34 ft 7 in)
  • Wing area: 121.7 m² (1,310 ft²)
  • Empty weight: 28,000 kg (62,000 lb)
  • Useful load: 60 paratroopers (two BMD-1 armoured vehicles)
  • Max. takeoff weight: 61,000 kg (130,000 lb)
  • Powerplant: 4 × Ivchenko AI-20L or AI-20M turboprops, 4,000 ehp (3,000 kW) each

Performance

  • Maximum speed: 777 km/h (419 knots, 482 mph)
  • Cruise speed: 670 km/h (361 knots, 415 mph)
  • Range:
    • With maximum fuel: 5,700 km (3,075 nm, 3,540 mi)
    • With maximum load: 3,600 km (1,945 nm, 2,235 mi))
  • Service ceiling: 10,200 m (33,500 ft)
  • Rate of climb: 10m/s (1960ft/min)

Armament

  • Guns: 2× 23 mm (0.906 in) Nudelman-Rikhter NR-23 cannons in a tail turret (some aircraft)

Nord 3202 Master

Nord 3202 Master F-AZIY/ZIY ex French Army

The Nord Aviation 3202 Master was a 1950s French military trainer aircraft designed and built by Nord Aviation to meet a French Army requirement for a two-seat basic trainer, as a replacement for the biplane Stampe SV.4.

  • Role: Two-seat trainer
  • National origin: France
  • Manufacturer: Nord Aviation
  • First flight: 17 April 1957
  • Retired: 1978
  • Status: Privately owned, or in museums
  • Operator: French Army
  • Number built: 101

Specifications (N 3202B)

General characteristics

  • Crew: two, pilot and instructor
  • Length: 8.12 m (26 ft 8 in)
  • Wingspan: 9.5 m (31 ft 2 in)
  • Height: 2.82 m (9 ft 3 in)
  • Wing area: 16.25 m² (175 ft²)
  • Empty weight: 860 kg (1,895 lb)
  • Maximum takeoff: 1,220 kg (2,690 lb)
  • Powerplant: 1 × Potez 4D34, 190 kW (260 hp)

Performance

  • Maximum speed: 260 km/h (160 mph)
  • Range: 1,000 km (620 mi)
  • Service ceiling: m ( ft)
  • Rate of climb: m/min ( ft/min)

 

Lockheed F-104 Starfighter

Lockheed F-104G Starfighter D-8030 ex Royal Netherlands Air Forc

The Lockheed F-104 Starfighter is a single-engine, supersonic interceptor aircraft originally developed by Lockheed for the United States Air Force (USAF).

  • Role: Interceptor aircraft, fighter-bomber
  • National origin: United States
  • Manufacturer: Lockheed
  • First flight: 17 February 1956
  • Introduction: 20 February 1958
  • Status: Retired 2004 Italy
  • Number built: 2,578
  • Developed from: Lockheed XF-104
  • Variants: Lockheed NF-104A, Canadair CF-104, Aeritalia F-104S

Operators

  • Belgium Air Force
  • Canadian Air Force
  • Danish Air Force
  • German Air Force
  • Hellenic Air Force (Greece)
  • Italian Air Force
  • Japan Self Defence Air Force
  • Jordanian Air Force
  • Royal Netherlands Air Force
  • Royal Norwegian Air Force
  • Pakistan Air Force
  • Republic of China Air Force (Taiwan)
  • Spanish Air Force
  • Turkish Air Force
  • United States Air Force

Specifications (F-104G)

General characteristics

  • Crew: 1
  • Length: 54 ft 8 in (16.66 m)
  • Wingspan: 21 ft 9 in (6.36 m)
  • Height: 13 ft 6 in (4.09 m)
  • Wing area: 196.1 sq ft (18.22 m²)
  • Airfoil: Biconvex 3.36% root and tip
  • Empty weight: 14,000 lb (6,350 kg)
  • Loaded weight: 20,640 lb (9,365 kg)
  • Max. takeoff weight: 29,027 lb (13,170 kg)
  • Powerplant: 1 × General Electric J79-GE-11A afterburning turbojet
    • Dry thrust: 10,000 lbf (48 kN)
    • Thrust with afterburner: 15,600 lbf (69 kN)
  • Zero-lift drag coefficient: 0.0172
  • Drag area: 3.37 sq ft (0.31 m²)
  • Aspect ratio: 2.45

Performance

  • Maximum speed: 1,328 mph (Mach 2.01, 1,154 kn, 2,137 km/h)
  • Combat radius: 420 mi (365 nmi, 670 km)
  • Ferry range: 1,630 mi (1,420 nm, 2,623 km)
  • Service ceiling: 50,000 ft (15,000 m)
  • Rate of climb: 48,000 ft/min (244 m/s)
  • Wing loading: 105 lb/(sq ft) (514 kg/m²)
  • Thrust/weight: 0.54 with max. takeoff weight (0.76 loaded)
  • Lift-to-drag ratio: 9.2

Armament

  • Guns: 1 × 20 mm (0.787 in) M61A1 Vulcan 6-barreled Gatling cannon, 725 rounds
  • Hardpoints: 7 with a capacity of 4,000 lb (1,814 kg) and provisions to carry combinations of:
    • Missiles: 4 × AIM-9 Sidewinder
    • Other: Bombs, rockets, or other stores

Piper PA-18 Super Cub

Piper PA-18-150 Super Cub HB-PAV/V-654 Swiss Air Force

The Piper PA-18 Super Cub is a two-seat, single-engine monoplane. Introduced in 1949 by Piper Aircraft.

  • Role: Light utility aircraft
  • Manufacturer: Piper Aircraft
  • First flight: 1949
  • Produced: 1949-1983; 1988-1994
  • Status: Active service
  • Number built: 15.000
  • Developed from: Piper PA-11

Military operators

  • Austrian Air Force
  • Belgian Army
  • Federal German Luftwaffe
  • Imperial Iranian Air Force
  • Italian Army
  • Israeli Air Force
  • Force Aérienne Katangaise
  • Netherlands Army
  • Nicaraguan Air Force
  • Japanese Army
  • Royal Norwegian Air Force
  • Portuguese Army
  • Portuguese Air Force
  • Swedish Army
  • Swiss Air Force
  • Turkish Army
  • Uganda
  • Uruguay
  • United States Air Force
  • United States Army

Specifications (PA-18-150 landplane)

General characteristics

  • Crew: 1
  • Capacity: 1 passenger
  • Length: 22 ft 7 in (6.88 m)
  • Wingspan: 35 ft 2½ in (10.73 m)
  • Height: 6 ft 8½ in (2.02 m)
  • Wing area: 178.5 sq ft (16.58 m²)
  • Airfoil: USA 35B
  • Aspect ratio: 7:1
  • Empty weight: 930 lb (422 kg)
  • Max. takeoff weight: 1,750 lb (794 kg)
  • Powerplant: 1 × Lycoming O-320 air-cooled flat four, 150 hp (112 kW)

Performance

  • Never exceed speed: 132 knots (246 km/h, 153 mph)
  • Maximum speed: 113 knots (208 km/h, 130 mph) at sea level
  • Cruise speed: 100 kts (185 km/h, 115 mph) (75% power)
  • Stall speed: 38 knots (69 km/h, 43 mph) flaps down
  • Range: 399 nmi (735 km, 460 mi)
  • Service ceiling: 19,000 ft (5,595 m)