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The Northrop Alpha


 

NACA Alpha
Photo: NASA

Northrop Alpha
Photo: Northrop Grumman

Northrop Alpha
Photo: Gerald Landry,
Graduate Aeronautical Laboratory,
California Institute of Technology (GALCIT)

Alpha Wind Tunnel Model
Photo: Graduate Aeronautical Laboratory,
California Institute of Technology (GALCIT)

Northrop Alpha
Photo: Northrop Grumman

Northrop Alpha X-2W
Photo: Northrop Grumman

Northrop Alpha NC942Y
Photo: Northrop Grumman

Northrop Alpha NC947Y
Photo: Northrop Grumman

Northrop Alpha - TWA No.8
1931

Northrop Alpha 2
Army Y1C-19, A.C.#31-516
Photo: USAF


Photos of Northrop Alpha NC11Y

Northrop Alpha - Marketing Brochure

Northrop Alpha - A Contemporary Description

Northrop Alpha - Wind Tunnel Research


History

Transcontinental & Western Air (which was to become TWA) was the launch customer and ordered 5 alphas. Those aircraft began services on April 20, 1931 from San Francisco to New York with 13 intermediate stops. The entire trip took just over 23 hours.

The Alpha had a multicellular wing of stressed skin construction. It was also first commercial type to be equipped with rubber deicer boots. A total of 17 Alphas were produced.


Specifications

Alpha - Model 2

Capacity:                              Pilot + 6 passengers
Powerplant:                        P&W R-1340 Wasp (420 hp)

Length: 28 ft 4-1/2 in Height: 9 ft Wingspan: 41 ft 10 in Wing Area: 295 sq ft Airfoil: Clark Y (18% at Root, 12% at tip)

Gross Weight: 4,500 lb Empty Weight: 2,590 lb Useful Load: 1,910 lb Payload with full fuel and 170 lb pilot: 940 lb Wing Loading: 14.4 lb/sq ft Power Loading: 10.7 lb/hp

Top Speed: 170 mph Cruising Speed: 145 mph Landing Speed: 60 mph Climb at Sea Level : 1400 fpm Climb at 10,000 ft : 650 fpm Time, SL to 10,000 ft: 10.5 min Service Ceiling: 19,300 ft Absolute Ceiling: 21,100 ft Takeoff Ground Roll: 535 ft Landing Ground Roll: 475 ft Fuel: 116 gal Oil: 13 gal Years Manufactured: 1930-31 Quantity Manufactured: 12 Certification: ATC 381

Alpha - Model 3

Capacity:                      Pilot + 2 passengers + Cargo
                                          or  Pilot + Cargo

Powerplant:                    P & W R-1340 Wasp C (420 hp)

Length: 28 ft 4-1/2 in Height: 9 ft Wingspan: 41 ft 10 in Wing Area: 295 sq ft Airfoil: Clark Y (18% at Root, 12% at tip)

Gross Weight: 4,500 lb Empty Weight: 2,679 lb Useful Load: 1,821 lb

Top Speed: 170 mph Cruising Speed: 145 mph Landing Speed: 60 mph Climb at Sea Level : 1400 fpm Climb at 10,000 ft : 650 fpm Climb SL to 10,000 ft: 10.5 min Service Ceiling: 19,300 ft Absolute Ceiling: 21,100 ft Takeoff Ground Roll: 535 ft Landing Ground Roll: 475 ft
Fuel: 116 gal Oil: 13 gal Years Manufactured: 1931 Certification: Group 2-335

Quantity Manufactured: 5 as original equipment. A number of Model 2's were converted to Model 3's by the factory.

Alpha - Model 4

Capacity:                                     Pilot + Cargo
Powerplant:                      P&W R-1340 Wasp C (420 hp)

Length: 28 ft 4-1/2 in Height: 9 ft Wingspan: 43 ft 10 in Wing Area: 312 sq ft

Gross Weight: 4,700 lb Empty Weight: 2,800 lb Useful Load: 1,900 lb

Top Speed: 177 mph Certification: ATC 451

Quantity Manufactured: None as original equipment. Most Model 3's were converted to the Model 4 configuration.

Alpha - Model 4a

Capacity:                                     Pilot + Cargo
Powerplant:                      P&W R-1340 Wasp C (420 hp)

Length: 28 ft 4-1/2 in Height: 9 ft Wingspan: 43 ft 10 in Wing Area: 312 sq ft

Gross Weight: 5,100 lb Empty Weight: 2,650 lb (2,660 for NC11Y as equipped) Useful Load: 2,450 lb

Top Speed: 177 mph Certification: ATC 461

Quantity Manufactured: None as original equipment. Most Model 4's were converted to the Model 4a configuration.


Links

Northrop Alpha (NASM Page)
The NASM (Smithsonian) Home of the Northrop Alpha
History of the GALCIT Ten-Foot Wind Tunnel

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