ppt about old indian airforce planes

1. Aero Ae-45
Role Utility aircraft
Manufacturer Aero
Vodochody, Let
First flight 21 July 1947
Primary users Czechoslovakia
China
Hungary
Soviet Union
Produced 1951-1963
Number built 590

2. Specifications (Aero 145)
General characteristics
•Crew: one, pilot
•Capacity: 3-4 passengers
•Length: 7.77 m (25 ft 6 in)
•Wingspan: 12.25 m (46 ft 21⁄2 in)
•Height: 2.30 m (7 ft 6 in)
•Wing area: 17.1 m² (184 ft²)
•Airfoil: Aero No. 58-64
•Empty weight: 960 kg (2,116 lb)
•Loaded weight: 1,500 kg (3,306 lb)
•Max. takeoff weight: 1,600 kg
(3,527 lb)
•Powerplant: 2 × Walter M 332-III air-
cooled 4-cylinder inline engine, 104
kW (140 hp) each
Performance
•Maximum speed: 282 km/h (152
knots, 175 mph)
•Cruise speed: 250 km/h (135 knots,
155 mph)
•Range: 1,700 km (918 nm, 1,055
miles)
•Service ceiling: 5,900 m (19,360 ft)
•Rate of climb: 5.0 m/s (985 ft/min)
•Wing loading: 88 kg/m² (18 lb/ft²)
•Power/mass: 0.08 kW/kg (0.05 hp/lb)

3. AS.10 Oxford
Role Training
aircraft
Manufacturer Airspeed Ltd
First flight 19 June 1937
Primary user Royal Air
Force
Number built 8,586
Developed
from
Airspeed
Envoy
Variants Airspeed

5. Antonov An-12
Role Civil and Military
transport aircraft
Manufacturer Antonov
First flight 16
December
[1]
1957
Introduction 1959
Status Active service
with various
airlines
(especially cargo)
and Air Forces
Primary users Belarus Air Force
Aeroflot
PLA Air Force
Produced 1957–1973
Number built 1,248
Developed from Antonov An-10
Variants Shaanxi Y-8

6. Specifications
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)
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)

7. Avro Anson
Role Multirole
aircraft,
primarily
a trainer
Manufacturer Avro
First flight 24 March
1935
Introduction 1936
Retired 28 June 1968
(RAF)
Primary users Royal Air
Force
Fleet Air Arm
Produced 1930s–1952
Number built 11,020

8. Specifications
General characteristics
•Crew: Three-four
•Length: 42 ft 3 in (12.88 m)
•Wingspan: 56 ft 6 in (17.22 m)
•Height: 13 ft 1 in (3.99 m)
•Wing area: 463 ft² (43.01 m²)
•Empty weight: 5,512 lb (2,500 kg)
•Loaded weight: 7,955 lb (3,608 kg)
•Max. takeoff weight: 8,500 lb (3,900 kg)
Performance
•Maximum speed: 188 mph (163 kn,
302 km/h) at 7,000 ft (2,100 m)
•Range: 790 mi (690 nmi, 1,271 km)
•Service ceiling: 19,000 ft (5,791 m)
•Rate of climb: 750 ft/min (3.8 m/s)
•Wing loading: 17.2 lb/ft² (83.9 kg/m²)
•Power/mass: 0.088 hp/lb (140 W/kg)

9. Dassault Ouragan
Role Fighter-
bomber
Manufacturer Dassault
Aviation
Designer Marcel
Dassault
First flight 28 February
1949
Introduction 1952
Retired 1980s
Primary users French Air
Force
Indian Air
Force
Israeli Air
Force
El Salvador Air
Force

11. Specifications
General characteristics
•Crew: One
•Length: 10.73 m (35 ft 2 in)
•Wingspan: 13.16 m (43 ft 2 in)
•Height: 4.14 m (13 ft 7 in)
•Wing area: 23.8 m² (256.2 ft²)
•Aspect ratio: 7.3:1
•Empty weight: 4,142 kg (9,132 lb)
•Loaded weight: 7,404 kg (16,323 lb)
•Max. takeoff weight: 7,900 kg
(17,416 lb)
•Powerplant: 1 × Rolls-Royce
Nene 104B turbojet, 22.2 kN
(4,990 lbf)
Performance
•Never exceed speed: Mach 0.83
•Maximum speed: 940 km/h (508 knots,
584 mph) (Mach 0.76) at sea level
•Cruise speed: 750 km/h (405 knots, 465
mph)
•Combat radius: 450 km (245 nm, 280 mi)
•Ferry range: 920 km (500 nm, 570 mi)
•Service ceiling: 13 000 m (42,650 ft)
•Rate of climb: 38 m/s (7,480 ft/min)
•Takeoff distance: 783 m (2,570 ft)
•Landing distance: 910 m (2,985 ft)

12. HAL Ajeet
Role Fighter
Manufacturer Hindustan
Aeronautics
Limited
First flight 1976
Introduction 1977
Retired 1991
Primary user Indian Air
Force
Number built 89 (including
10 upgraded
Gnats)
Developed
from
Folland Gnat

13. Specifications
General characteristics
•Crew: 1
•Length: 9.04 m (29 ft 8 in)
•Wingspan: 6.73 m (22 ft 1 in)
•Height: 2.46 m (8 ft 1 in)
•Wing area: 12.69 m² (136.6 ft²)
•Aspect ratio: 3.56
•Empty weight: 2,307 kg (5,086 lb)
•Loaded weight: 3,539 kg (7,803 lb)
clean take-off weight
•Max. takeoff weight: 4,173 kg
(9,200 lb)
•Powerplant: 1 × TJE HAL/Bristol
Siddeley Orpheus 701-01 turbojet,
20.0 kN (4,500 lbf)
Performance
•Maximum speed: 1,152 km/h (622 knots,
716 mph) at sea level
•Combat radius: 172 km (93 nmi, 107 mi)
low level, with two 250 kg bombs
•Service ceiling: 45,000 ft (13,720 m)
•Wing loading: lb/ft² (kg/m²)
•Climb to 12,000 m (39,375 ft): 6 min 2 s

14. Specifications (HAL Ajeet)
General characteristics
•Crew: 1
•Length: 9.04 m (29 ft 8 in)
•Wingspan: 6.73 m (22 ft 1 in)
•Height: 2.46 m (8 ft 1 in)
•Wing area: 12.69 m² (136.6 ft²)
•Aspect ratio: 3.56
•Empty weight: 2,307 kg (5,086 lb)
•Loaded weight: 3,539 kg (7,803 lb) clean take-
off weight
•Max. takeoff weight: 4,173 kg (9,200 lb)
Performance
•Maximum speed: 1,152 km/h (622 knots, 716
mph) at sea level
•Combat radius: 172 km (93 nmi, 107 mi) low level,
with two 250 kg bombs
•Service ceiling: 45,000 ft (13,720 m)
•Wing loading: lb/ft² (kg/m²)
•Climb to 12,000 m (39,375 ft): 6 min 2 s