Convair F-106 Delta Dart

· Convair

Airplanes

Length

21.55 m

Flat Wing Span

11.67 m

Height

6.18 m

Flat Wing Area

61.4554 m²

Flat Wing Aspect Ratio

2.1

Max Speed

2453.898 km/h

Max Mach

2.3 Mach

Max Ceiling

17373.6 m

Number of Engines

First Flight

1956-12-26

Entry Into service

1959-06-01

Number Built

342

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Aircraft
Convair F-106 Delta Dart

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Convair F-102 Delta Dagger		20.7264	11.5824	Compare
Yakovlev Yak-201	Saturn AL-31	19	11.7	Compare
North American F-107	Pratt & Whitney J75	18.85	11.15	Compare
Sukhoi P-1		21.3	9.8	Compare
Republic XF-103	Rolls-Royce Olympus	23.5	10.5	Compare
CAMS 120		17.3	11.6	Compare

All data (23 fields)

Name: Convair F-106 Delta Dart
Manufacturer: Convair
Description: The Convair F-106 Delta Dart is an all-weather interceptor aircraft designed and produced by the American aircraft manufacturer Convair, a division of General Dynamics.
First Flight: 1956-12-26
Entry Into service: 1959-06-01
Service End: 1988-08-01
Designer: Convair
Length (m): 21.55
Height (m): 6.18
Cockpit Crew: 1
Max Speed (km/h): 2453.898
Max Ceiling (m): 17373.6
Rate of Climb (m/s): 147.32
Armament: 1 × 20 mm caliber M61A1 Vulcan 6-barreled rotary cannon (Available after 1972 refit); 2 × AIM-4F Falcon and 2 × AIM-4G Falcon; 1 × AIR-2A Genie nuclear-armed rocket (Not available later with M61A1)
Max Mach (Mach): 2.3
Number Built: 342
Powerplant Description: 1 × Pratt & Whitney J75-P-17 afterburning turbojet engine
Primary Users: United States Air Force, Air National Guard
Wikipedia Article (URL): en.wikipedia.org/wiki/Convair_F-106_Delta_Dart
Flat Wing Span (m): 11.67
Flat Wing Area (m²): 61.4554
Flat Wing Aspect Ratio: 2.1
Number of Engines: 1