Lockheed L-2000 Starcatcher

From Shipbucket Wiki
Revision as of 17:53, 27 October 2024 by The Sprinklez (talk | contribs) (Created page; added wikibox; categorized page)
(diff) ← Older revision | Latest revision (diff) | Newer revision → (diff)
Jump to: navigation, search
Lockheed L-2000 Starcatcher
Role Wide-body jet airliner
National origin United States of America
Manufacturer Lockheed Corporation
First flight 5 August 1988
Introduction 1989
Status In service
Produced 1975-1977
Number built 5
Developed from Lockheed L-1011 TriStar

The Lockheed L-2000 Starcatcher is an American medium-to-long-range, wide-body twinjet airliner built by the Lockheed Corporation as a successor to their L-1011 Tristar.

Design and Development

Operational History

Variants

  • L-2000-100
  • L-2000-150
  • L-2000-200

Operators

Specifications (U-26A)

General Characteristics:
Crew:
Capacity:
Length:
Wingspan:
Height:
Empty Weight:
Max Takeoff Weight:
Powerplant:


Performance:
Never-Exceed Speed (Vne):
Cruise Speed:
Stall Speed, Landing Configuration (Vso):
Range:
Service Ceiling:
Rate of Climb:
Takeoff Run:
Landing Run:

See also

Related Development