Douglas D-558-2 Skyrocket

Length
12.8016 m
Flat Wing Span
7.62 m
Height
3.6576 m
Flat Wing Area
16.258 m²
Max Speed
941.4662 km/h
Number of Engines
1
First Flight
1948-02-04
Number Built
3
Total Fuel Capacity
946.3529

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Aircraft Weight Variants

Aircraft Total Fuel Capacity
Douglas D-558-2 Skyrocket 946.3529

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All data (19 fields)
Name
Douglas D-558-2 Skyrocket
Manufacturer
Douglas Aircraft Corporation
Description
The Douglas D-558-2 Skyrocket (or D-558-II) is a rocket and jet-powered research supersonic aircraft built by the Douglas Aircraft Company for the United States Navy.
First Flight
1948-02-04
Designer
Douglas Aircraft Corporation
Type
Experimental high-speed research aircraft
Length (m)
12.8016
Height (m)
3.6576
Cockpit Crew
1
Max Speed (km/h)
941.4662
Min Speed (km/h)
257.495
Rate of Climb (m/s)
113.792
Number Built
3
Powerplant Description
1 × Westinghouse J34-WE-40 turbojet engine
Primary Users
United States Navy
Wikipedia Article (URL)
en.wikipedia.org/wiki/Douglas_D-558-2_Skyrocket
Flat Wing Span (m)
7.62
Flat Wing Area (m²)
16.258
Number of Engines
1