Lockheed C-141 Starlifter

Airplanes

Length

51.3 m

Flat Wing Span

48.8 m

Height

12 m

Flat Wing Area

300 m²

Max Speed

912 km/h

Max Ceiling

12500 m

Number of Engines

Aircraft Engine

First Flight

1963-12-17

Entry Into service

1965-04-01

Number Built

285

Maximum Take-Off Weight

147 t (paragliders: kg)

Maximum Range

4723 km

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Lockheed C-141 Starlifter	147	4723

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Myasishchev VM-T		51.23	53.14		Compare
Vickers VC10	Rolls-Royce Conway	48.1584	44.5008	151	Compare
Boeing CC-137	Pratt & Whitney JT3D	46.61	44.42	170	Compare
Boeing C-137 Stratoliner		46.61	44.42		Compare
Xi'an H-8		48.5	46.47		Compare
Northrop Grumman E-8 Joint STARS	Pratt & Whitney JT3D	46.61	44.42		Compare

All data (27 fields)

Name: Lockheed C-141 Starlifter
Manufacturer: Lockheed Corporation
Description: The Lockheed C-141 Starlifter is a retired four-engine military strategic airlifter that served with the Military Air Transport Service (MATS), its successor organization the Military Airlift Command (MAC), and finally the Air Mobility Command (AMC) of the United States Air Force (USAF).
ICAO Code: C141
First Flight: 1963-12-17
Entry Into service: 1965-04-01
Production End: 1968-01-01
Service End: 2006-05-01
Designer: Lockheed Corporation
Type: Strategic airlifter
Length (m): 51.3
Height (m): 12
Cockpit Crew: 5
Max Speed (km/h): 912
Max Ceiling (m): 12500
Rate of Climb (m/s): 13.2
National Origin: United States of America
Number Built: 285
Powerplant Description: 4 × Pratt & Whitney TF33-P-7 turbofans, 90.1 kN thrust each
Primary Users: United States Air Force, NASA
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Lockheed_C-141_Starlifter
Flat Wing Span (m): 48.8
Flat Wing Area (m²): 300
Wake Category: H
Aircraft Engine: Pratt & Whitney JT3D
Number of Engines: 4