WesWorld

Heinkel sees no difficulty in opening a production line for the He-111E at Heinkel Ost. Jumo's development of the Jumo-211G will allow that more powerful engine to be fitted to the He-111E, resulting in the E-6 version (equivalent to the historical H-6 version).

How many Fw-187 P-6s would the Phillipines like?


For the VHB requirement, Consolidated Aircraft proposes the new B-24.

Bomber:

E.W.I.L. EW 208 C "Flying Dragon"
Heavy Bomber
Range: ~ 6000km
Bombload: up to 5000kg


Guizhou GA-5
Heavy Bomber
Range: ~ 6000km
Bombload: up to 6000kg


Shanxi: SH-15
Medium Bomber
Range: 3200km
Bombload: ~ 1500kg


Transporter:

SAC-52
Transporter
17 passengers or 3900kg
Range 1200km


ROC-14
Transporter
34 passengers or 4500kg
Range: 3000km


For detailed info the chinese encyclopedia.

Very Heavy Bomber

Kanzaki Ki-70 Bomber

Stats on previous page.


Scout/Reconnasiance Aircraft

Mitsubishi Ki-16

Stats on previous page (C5)

Tachikawa Ki-41

Crew: 2
Length: 8.00 m
Wingspan: 11.80 m
Height: 3.64 m
Empty weight: 1247 kg
Max takeoff weight: 1660 kg
Powerplant: Hitachi Ha-13a, 515 hp
Maximum speed: 348 km/h
Service ceiling: 8150 m
Range: 1235 km
Armament: Two 7.7mm machine guns, 150 kg bombs

For the Army Cooperation Aircraft, Focke-Wulf proposes the Fw-189.

For the Very Heavy Bomber, Junkers proposes a version of the Ju-90S, re-engined with the Jumo-211 J and uparmored and armed in light of the events in South America.


Aircraft Type or Name:

Junkers Ju-90P

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

Year of First Flight: 1938

Description

Conventional Aircraft
Monoplane
Conventional Fuselage


A Jumo-powered version of the Ju-90S. Armed with a single 15mm MG-151 in the dorsal turret and the rear of the ventral gondola, and twin 7.92mm MG-81Zs in the nose and beam positions. Protection includes 900 lbs of 10mm armor plate around the cockpit, and self-sealing fuel tanks (2400 lbs). Can carry a bomb load of up to 5000 kg over a range of up to 2000 nm.


Characteristics:

Weight (maximum) 66,000 lbs
Weight (empty) 35,810 lbs

Length 71.5 ft
Wingspan 115 ft
Wing Area 1,944 sq ft
Sweep 1 degrees

Engines 4
Jumo-211 J
Piston

1,348 hp
at 12,000 ft


Crew 6


Typical cost $0.146 million in 1939
Total number procured 2000


Performance:

Top Speed 244 kts = 281 mph
at 12,000 ft
Mach N/A

Operational Ceiling 26,500 ft

Range 2,000 nm = 2,303 miles
with 12,592 lbs payload
14,481 lbs released at halfway point

Climb 875 fpm

Cruise 185 kts = 213 mph
at 20,000 ft

Corner Speed 168 KIAS =
201 kts at 12,000 ft
Mach N/A
Turning Rate 18.1 deg/sec
Radius 2,174 ft



Internal Data:

Intake / Fan Diameter 10.5 ft

Bypass Ratio 93

Engine Weight 1940 lbs
Overall Efficiency 22.5 percent

Structural Factor 0.98

Number of Wings 1
Number of Fuselages 1

Limiting Airspeed 275 kts
Wing Ultimate g Load 4.00 g
Wing Taper 0.2
Wing Thickness at Root 3.4 ft

Tail / Canard Factor 0.4

Number of Nacelles 4
Length 12 ft
Diameter 3.25 ft
Fullness 0.5

Fuselage Diameter 8 ft
Fuselage Fullness 0.5

Pressurized Volume 0 percent
Cargo Decks 0

Cleanness 65 percent
Unstreamlined section 4.8 sq ft

User equipment 6,300 lbs

Great Britain's industries striving to improve exports answer the call for modern and advanced aircrafts!

For Army Co-Operation:
Westland P.8 Lysander Mk II; This two-seater uses full-span leading edge slots to achieve a remarkable short take-off and landing performance. Armament is two 7.62-7.92mm machineguns in the undercarriage spats and two light MG in the rear cockpit. 240lbs of bombs or supply packs can be carried on stub wings fixed to the undercarriage spats.
Dimensions; 50/ 30.6/ 14.6/ 260 sq ft; 1x 905hp Bristol Perseus XII; max speed 230 mph, range 600 miles and service ceiling 21,500ft.

For transport;
de Havilland D.H.95A Hertfordshire; based on the D.H.95 Flamingo airliner with space for eighteen troops. Dimensions; 70/ 51.7/ 15.3/ 651 sq ft; 2x 930hp Bristol Perseus XVI; max speed 243mph; range 1,345 miles and service ceiling 20,900ft.
[Note these will be built by de Havilland Australia]

I usually don't offer planes to any SATSUMA tenders, but Chile's got the Condor line...

Valdivia Condor:
Length: 28.5 feet
Wingspan: 44 feet
Height: 8 feet
Wing area: 275.15 ft²
Weight: 1,200 pounds
Crew: One pilot, three passengers
Speed: 87 knots (100mph)
Rate of climb: 600 feet per minute
Ceiling: 15,000 feet
Range: 250-300 miles (engine dependent)
Powerplant: De Havilland Gipsy Minor (90hp), Gipsy Major (130hp), Gipsy Six (200hp), or Canadian Orenda engines
Remarks: parasol wing, taildragger

Valdivia Twin Condor:
Length: 47 feet
Wingspan: 59 feet
Height: 16 feet
Wing area: 410 ft²
Weight: 5,520 pounds
Crew: One pilot; 16 passengers
Speed: 150 knots (172mph)
Rate of climb: 1,100 feet per minute
Ceiling: 18,000 feet
Range: 700 nautical miles (engine dependent)
Powerplant: Gipsy Six (200hp), or Canadian Orenda engines
Remarks: Parasol wing, fixed tricycle gear

((No, the versions available don't meet Philippine requirements, as they were constructed to my requirements... ))