Curtiss Conqueror V-1570, V-12 Engine

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Display Status:

This object is not on display at the National Air and Space Museum. It is either on loan or in storage.

Collection Item Summary:

The Conqueror developed from a history of Curtiss engines beginning in the early twentieth century. It was the last of Curtiss liquid cooled engines. The U.S. Navy purchased this engine in 1930 and installed it in the Curtiss XF6C-6 Hawk, a biplane converted to a monoplane racer. On September 1, 1930, U.S. Marine Corps pilot Capt. Arthur H. Page Jr., flew the aircraft in the Thompson Trophy Air Race in Chicago. While leading the field, the aircraft lost power, and Page died during the resulting forced landing.

To determine what happened, the Navy's Aeronautical Engine Laboratory disassembled and inspected the engine. They determined that the magneto drive shaft bushing and housing failed, which most likely retarded the magneto timing enough to cause a loss of power and engine failure. While historians have speculated that Page was overcome by fumes and crashed, the official Navy report indicated otherwise.

Collection Item Long Description:

Date

July 7, 1930

Inventory Number

A19710913000

Physical Description

  • Type: Reciprocating, V-type, 12 cylinders, Liquid-cooled
  • Power Rating: 500 kW (670 hp) at 2,405 rpm
  • Displacement: 25.7 L (1,570 cu in.)
  • Bore and Stroke: 130 mm (5.1 in) x 159 mm (6.2 in)
  • Weight: 493.5 kg (1,088 lb)

Credit Line

Transferred from the U.S. Navy

Country of Origin

United States of America

Materials

Aluminum, Steel, Rubber, Stainless Steel, Magnesium

Dimensions

Overall: 3 ft. 11 in. × 2 ft. 5 5/8 in. × 5 ft. 4 in., 1088lb. (119.4 × 75.2 × 162.6cm, 493.5kg)

Data Source

National Air and Space Museum

Restrictions & Rights

Do not reproduce without permission from the Smithsonian Institution, National Air and Space Museum

Type

PROPULSION-Reciprocating & Rotary