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Saab 105 Oe (in Schweden: SK 60)
Typ: Strahltrainer, Erdkampfflugzeug
Hersteller: Saab AB, Linköping, Schweden (heute Saab Aerosystems)
Besatzung: 2 (+2 bei Verwendung des Umrüstsatzes)
Leermasse: 3.085 kg
max. Startgewicht: 5.700 kg
Länge: 10,80m / Spannweite: 9,50m / Höhe: 2,70m /
Flügelfläche: 16,30 m²
Triebwerke: 2x General Electric J85-17B mit je 12,68kN (1.294kg)
Schubkraft-Gewichts-Verhältnis: -
Tankinhalt: 2.550 Liter
Geschwindigkeit: max. 970 km/h
Steigfähigkeit: 75 m/s
max. Lastvielfaches: -3g bis +6g
Aktionsradius: ca. 850 km / Überstellreichweite: 2770 km
mit zwei 490 Liter Zusatztanks
Dienstgipfelhöhe: 13.100 m
Pistenerfordernis: -
Radar: keines
Ausstattung: 2 Schleudersitze oder 4 normale Sitze (2 Umbausets),
tragbare GPS Moving Map, 490 Liter Zusatztanks, 8 Radiak-Behälter
zur Entnahme von Luftproben; bis November 1992: 8 Vinten-Kamera-Pods
(je 5 VINT 360 Kameras)
Bewaffnung: 2x 30mm Maschinenkanonen MATRA SA-10 ADEN Mk4 (in
Kanonenbehältern, je 150 Schuss), früher: bis zu 12 ungelenkte
75mm Raketen, Maximal 750 kg Außenlasten an sechs Flügelstationen.
Saab 105 Oe (SK 60 in Sweden)
Jettrainer, VIP-Transport. The Saab 105 Oe is a variant of the Saab
105 XT. Over a long period of time, the 40 Saab 105 were the backbone
of the Austrian Air Force. Today the aircraft is mainly used as a Jettrainer,
but it is also used for the protection of major events (against slow
targets) and for VIP transports. For liaison duties, the 2 ejection
seats can be exchanged for 4 normal seats.
Austria is partner country of the Advanced
European Jet Pilot Training (AEJPT) program. The future of Austria's
own Jettrainers is therefore uncertain. Plans have been made to upgrade
16 to 22 Saab 105 with glass cockpits and to put the remaining planes
out of service. But the aquisition of used jet trainers is more certain.
Manufacturer: Saab AB, Linköping, Sweden (today Saab Aerosystems)
Crew: 2 (+2 in transport configuration)
Weight empty: 3.085 kg
Max. Take-off Weight: 5.700 kg
Length: 10,80m / Wingspan: 9,50m / Height: 2,70m
/
Wing area: 16,30m²
Engines: 2x General Electric J85-17B with 2x 12,68kN (1.294kg)
Thrust to Weight Ratio: -
Internal Fuel Tanks: 2.550 liters
Maximum Speed: 970 km/h
Climbing Rate: 75 m/sek.
G-limits: -3 to +6 g
Range: Radius of action: 850 km / transfer range: 2.770 km with
two external tanks.
Service Ceiling: 13.100 m
Operational Runway Length: -
Radar: none
Equipment: 2 Ejection Seats or 4 normal seats (2 kits),
portable GPS Moving Map, 490 Liters external fuel tanks, 8 Radiak-Pods
for taking air-probes, in the uptto November 1992: 8 Vinten-Film-Camera-Pods
(5 VINT 360 cameras each).
Armament: 2x 30mm Machine Cannons MATRA SA-10 ADEN Mk4 (in external
pods with 150 rounds each), in the past: up to 12 unguided 75mm A2G-Missiles,
max 750 kg Payload on 6 Hardpoints.
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