Lockheed L-2000 Starcatcher
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| 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.
Contents
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
