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21

Wednesday, January 24th 2018, 3:23pm

Gangchuan F-5

Gangchuan F-5
Gangchuan Aviation Ltd.
Type: Heavy Fighter

Engine:
Two DB600

Speed / ceiling / range:
Maximum Speed: 404km/h (251 mph)
Initial climb: N/A
Service Ceiling: 29,855 ft. (9100m)
Range: n.n.

Weight:
Empty: 6,800kg (14,991 lbs.)
Maximum: 8,300kg (18,298 lbs.)

Dimensions:
Wing span: 25m (82 ft. 0 in.)
Length: 16.40m (53 ft. 9.5 in.)
Height: 4.08m (13 ft. 5.25in.)
Wing Surface Area: N/A Weights:

Armament:
Two manually aimed 20mm MG FF Cannon mounted in the
nose plus a third in a Mauser electric dorsal turret.

Bombload:
Six 220lb. (100kg) bombs in internal bomb bay.

Crew:
Crew: 3



22

Wednesday, January 24th 2018, 3:25pm

Shaanxi SH-45

Shaanxi SH-45
Shaanxi Aviation Ltd.
Long Range Fighter

Engine:
2x Mitsubishi Ha-102, 1080 hp

Speed / Ceiling / Range:
max. speed: 540 kph
cruise speed:
ceiling: 10730 m
range: 2260 km

Weight:
empty weight: 4.000 kg
max take off weight: 5.500 kg

Dimensions:
length: 11.00 m
height: 3.70 m
wingspan: 15.05 m
wingarea: 32.00 m²

Armament:
SH-45A:
1x 20mm machine cannon lower right forward fuselage
2x 17.7mm machine guns fixed in nose
2x 7.92mm machine guns

SH-45B:
1x 37mm machine cannon
1x 20mm machine cannon
2x 7.92mm machine guns

SH-45C:
Two 12.7mm machine guns fixed in nose
Two 7.7mm machine guns manually aimed from rear cockpit

Bombload:
2x 200 liter drop tanks or
external up to 500 kg

Crew:
2 men



23

Wednesday, January 24th 2018, 3:26pm

Guoyong G35-A

Guoyong G35-A
Guoyong Aircraft Inc.
Type: Flightboat

Engine:
2 radial Huang-Po with 950hp

Speed / Ceiling / Range:
Max Speed / Alt: 167 kn / 5800 ft
service ceiling: 19700 ft
Range: 760 nm

Weight:
Empty: 6415 lbs
Basic: 6766 lbs
Max: 8700 lbs

Dimensions:
Span: 49' - 0"
Length: 38' - 4"
Height: 4' - 7"

Armament:
None

Load:
4 Passengers

Crew:
2 men (pilot, Co-pilot {radio-operator})



24

Wednesday, January 24th 2018, 3:28pm

Harbin 35

Harbin 35-B (License build of the Do-18 )
Harbin Aircraft Manufacturing Corporation
Type: Flightboat

Engine:
2x Jumo 205C (Diesel engine), 600hp (440kW)

Speed / Ceiling / Range:
Maximum Speed: 260km/h (162 mph)
Initial climb: N/A
Service Ceiling: 4200m (13800 ft)
Range w/max. fuel: 5100km (3169miles)
Range w/max. payload: 2600km (1616miles)

Weight:
Empty: 6260kg (13801 lbs.)
Maximum: 10000kg (22046 lbs.)

Dimensions:
Wing span: 23,7m (77 ft. 9 in.)
Length: 19,3m (63 ft. 4 in.)
Height: 5,4m (17 ft. 9in.)
Wing Surface Area: 98,0 m² 1054,86 sq ft.

Armament:
None

Load:
None

Crew:
4 men



25

Wednesday, January 24th 2018, 3:32pm

Dornier Do-24C

Here's the version that the Chinese Air-Sea Rescue Service has bought. The listed payload is to carry raft bundles
under the wings for situations where either the seas are too rough for the plane to land, or there are more people
in the water than the plane can rescue.

Aircraft Type or Name:

Dornier Do-24C

General Type:
Airplane = 1
Airship = 2
Orbiter = 3
1

Year of First Flight: 1935

Description

Flying Boat / Seaplane
Monoplane
Conventional Fuselage

A Jumo-208 powered version of the historical Do-24A. Lower fuel consumption will result in a max range of 3000 miles
vs the listed 2400 nm. Unarmed rescue aircraft, designed to carry 6 passengers.


Characteristics:

Weight (maximum) 36,300 lbs
Weight (empty) 18,481 lbs

Length 71.5 ft
Wingspan 89 ft
Wing Area 1,148 sq ft
Sweep 5 degrees

Engines 3
Jumo 208A
Piston

1,211 hp
at 8,000 ft


Crew 5


Typical cost $0.089 million in 1939
Total number procured 120


Performance:

Top Speed 234 kts = 269 mph
at 8,000 ft
Mach N/A

Operational Ceiling 20,000 ft

Range 2,400 nm = 2,764 miles
with 4,931 lbs payload
5,982 lbs released at halfway point

Climb 1,338 fpm

Cruise 160 kts = 184 mph
at 8,000 ft

Corner Speed 117 KIAS =
132 kts at 8,000 ft
Mach N/A
Turning Rate 13.7 deg/sec
Radius 1,867 ft



Internal Data:

Intake / Fan Diameter 10 ft

Bypass Ratio 95

Engine Weight 1750 lbs
Overall Efficiency 23 percent

Structural Factor 0.95

Number of Wings 1
Number of Fuselages 1

Limiting Airspeed 250 kts
Wing Ultimate g Load 2.50 g
Wing Taper 0.1
Wing Thickness at Root 2.4 ft

Tail / Canard Factor 0.2

Number of Nacelles 3
Length 6 ft
Diameter 3 ft
Fullness 0.5

Fuselage Diameter 9 ft
Fuselage Fullness 0

Pressurized Volume 0 percent
Cargo Decks 0.5

Cleanness 60 percent
Unstreamlined section 8.5 sq ft

User equipment 2,000 lbs