Stampe and Vertongen Museum
April 24, 2009 by R.Vogelaar · Leave a Comment

Stampe and Vertongen Museum
Luchthavenlei
Luchthaven Antwerpen-Deurne
Belgium
Airbus A400M
November 19, 2008 by Marcel van Leeuwen · Leave a Comment
The A400M program is a direct result of a commonly expressed need by 8 European air forces for a new generation military airlifter.
Airbus A400M timeline:
The Airbus A400M development started in the seventies as the Future Large Aircraft project. Request for Proposal August 1997.
Memorandum of Understanding is signed June 19, 2001 at the Le Bourget Air show.
On May 27, 2003, a contract was signed between Airbus Military and OCCAR (Organization Conjointe de Coopération en Matière d’Armement), representing Belgium, France, Germany, Luxembourg, Spain, Turkey, and United Kingdom for a total of 180 aircraft.
The industrial program was formally launched on May 31, 2003.
Start production January 2005.
First Roll out: June 26, 2008
First Flight December 11, 2009, and the first deliverywill be in 2012.

First Flight December 11, 2009
The A400M Common Standard Aircraft (CSA) is capable of performing:
strategic operations (long range, large capacity, high cruise speed).
tactical missions (soft-field performance, autonomous ground operation, low speed / low level operations, aerial delivery).
“in-theatre” tanking operations (receiving as well as dispensing fuel).
The A400M is designed to civil certification standards complemented where appropriate by specific military requirements. The aircraft design incorporates leading state-of-the-art technology including:
Fly-by-wire Flight Control System with side stick controllers.
Flight envelope protection system, already proven in Airbus commercial aircraft.
Advanced structural design incorporating extensive use of composite materials.
High performance turboprop engines, allowing operation in civil air traffic control environment.
High flotation landing gear, allowing operation from short, unpaved airfields.
The Airbus A400M will play an essential role in enhancing Europe’s airlift capabilities, whilst enabling the establishment of common support, training and operational procedures and greater interoperability in multi-national humanitarian and peace-keeping missions.
Air-to-Air Refueling:
The A400M is also quickly convertible into a tactical tanker. The flight envelope of the A400M allows it to refuel a wide range of aircraft and helicopters, at the altitudes appropriate to their missions.
A two-point trailing drogue system can be installed within two hours by fitting two standard air-to-air refueling pods (optional) to the multi-role attachment points on the wings. Each pod provides a fuel flow of up to 1200kg/min.
A centre-line pallet-mounted hose drum unit can be fitted in the rear cargo bay. It provides a fuel flow of 1800kg/min.
| Developing nation: | European Nations. |
| Manufacturer/designer: | Airbus Military. |
| Production line: | Sevilla, Spain |
| Type aircraft: | Military transporter. |
| First flight: | December 11, 2009 |
| First delivery: | 2012 |
| Airbus A400M | |
| Cockpit crew: | 2 pilots, 1 loadmaster |
| Troops: | 120 |
| Cabin length: | 17,71 m. |
| Cabin diameter: | 4,00 m. |
| Cabin height: | 3,85 m. |
| Ramp length: | 5,40 m. |
| Cargo volume: | 356 m³. |
| Wing span: | 42,4 m |
| Wing area: | 221,5 m². |
| Fuselage length: | 43,8 m. |
| Fuselage diameter: | 4,10 m. |
| Height: | 14,6 m. |
| Engines: | - four Europrop International TP400-D6 each rated 11.000 Hp. |
| Propeller: | Ratier FH386 eight blades 5,33 m diameter. |
| Weight: | - empty: 70.000 Kg.- fuel: 46.700 kg.- max. payload: 37.000 Kg. |
| Max. take off weight: | 130.000 Kg. |
| Max. landing weight: | 114.000 Kg. |
| Cruise speed: | mach 0,68. |
| Max. speed: | mach 0,72. |
| Service ceiling: | 8.840 m. |
| Max. ceiling: | 12.190 m. |
| Max. range: | 9.260 km. |
| Performance: | - take-off run 940 m at max. take-off weight.- landing run 625 m at max. landing weight. |
| Airbus A400M order book: | |
| BelgiumChileFrance
Germany Luxembourg Malaysia Spain Turkey United Kingdom |
7350
60 1 4 27 10 25 |
Dassault Dornier Alpha Jet
October 22, 2008 by Marcel van Leeuwen · Leave a Comment
The Dassault Dornier Alpha Jet is a French / German jet trainer and strike aircraft. The French version is a trainer, and the German version primarily a strike aircraft. The Alpha Jet is a twin engine aircraft with a high-site, moderately wing.
German Alpha Jets were flown almost exclusively as single-seat close support weapons trainer, or battlefield reconnaissance aircraft. Weapons load and avionics do not match those of more advanced jets, but the Alpha Jet is maneuverable, easy to fly and simple to maintain. It’s equipment allows it to obtain great efficiency when planning and executing missions.
The Head Up Display (HUD) saves the pilot from looking down in the cockpit to read the instruments, by superimposing data on a clear plate mounted at the pilot’s eye level.
The naviagtion and fire control computers are rather precise and permit a great flexibility on attack missions, the use of AFA computer makes it simpler, quicker and more efficient to plan a mission. There is also other equipment that allows the crew members to have a good combat survivability.
- Belgian AF Alpha Jet AT-08
- Belgian Alpha Jet, AT-28
- Portugese Alpha Jet
- Belgian Alpha Jets Taxiing
- Belgian Alpha Jet AT-18
- Belgian Alpha Jet, AT-29
- French Alpha Jet, E105-8 NU
- French Alpha Jet Cockpit close up.
- Three Belgian Alpha Jet’s in Formation
NB. The Alpha Jet A has a ’sharper nose’ then the Alpha Jet E
| Developing Nation: | France and Germany |
| Task: | Trainer / strike and close support |
| First Flight: | - Alpha Jet A: January 9th 1974 (D-9594)- Alpha Jet E: October 26th 1973 (F-WZRO) |
| Prototypes: | - Alpha Jet A:02/D-9594 (ff: January 9th 1974)04/D-9595 (ff: October 11th 1974 crashed 23 January 1976)- Alpha Jet E:
F-WZRO (ff: October 26th 1973) F-WZRV (ff: May 6th 1974 ) |
| First Delivery: | - French Air Force: May 4th 1979- Luftwaffe: March 20th 1980 |
| Crew: | 2 |
| Ejection seat: | |
| Wing Span: | 9,11 m |
| Length: | - Alpha Jet A: 13,23 m- Alpha Jet E: 12,29 m |
| Height: | |
| Engine (s): | - Alpha Jet A: GRTS (SNECMA Turbomeca) Lazarc 04-C20 (2x)- Alpha Jet E: GRTS (SNECMA Turbomeca) Lazarc 04-C6 (2x) |
| Weight: | 3515 kg |
| Max.Take off weight: | 6100 kg |
| Max. Speed: | 917 km/h |
| Max. Range: | - Just on internal fuel: 2780 km (1900 liters)- With extra external fuel: 4000 km (extra 600 liters) |
| Operation altitude: | 14630 m |
| Weapons: | - Mauser BK.27 cannon or DEFA 553 gun-pod- AIM-9 Sidewinder- R.550 Magic II- AGM-65 Maverick
- GP Bombs - Hunting BL755 cluster bombs -Matra RL F4 - Rockets & Bomb rack SUU 20A - BLG-66 Belouga - Bombs MK82 ‘Snake Eye’ - Exercise bombs MK106 - Bombs BLU-1CB |
| Extra: |
Countries who use(d) the Alpha Jet:
|
Belgium |
33 Alpha Jet E |
|
Cameroon |
7 Alpha Jet MS2 |
|
Egypt |
30 Alpha Jet MS1 & 15 MS2 |
|
France |
175 Alpha Jet E |
|
Germany |
175 Alpha Jet A |
|
Ivory coast |
12 Alpha Jet E |
|
Maroc |
24 Alpha Jet E |
|
Nigeria |
24 Alpha Jet E |
|
Portugal |
50 Alpha Jet A ** |
|
Qatar |
6 Alpha Jet E |
|
Thailand |
20 Alpha Jet A ** |
|
Togo |
5 Alpha Jet E |
|
United Kingdom |
12 Alpha Jet A ** |
** Ex German Air Force

















