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Development of Requirement, Configuration and Design for the Lockheed 1011 Jet Transport
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English
Abstract
Successful development of a commercial transport airplane depends primarily on satisfying three fundamental aspects: safety, economics, and community acceptance. In turn, these factors are heavily influenced by the airplane configuration, operational characteristics, and engineering design features. This paper presents some of the major considerations leading to the development of the L-1011 configuration selection, and the operating requirements used in establishing the basic design of the airplane.
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Citation
Magruder, W., "Development of Requirement, Configuration and Design for the Lockheed 1011 Jet Transport," SAE Technical Paper 680688, 1968, https://doi.org/10.4271/680688.Also In
References
- “Aircraft Operators Council Aeronautical Requirements Handbook,” December 1965
- “Handling Qualities Data for Various Aircraft Compared to Present and Proposed Criteria,” Lockheed Report LR 20164 June 1968
- “Design Objectives for Flying Qualities of Civil Transport Aircraft,” SAE ARP 842A Aug. 15 1966
- “Airworthiness Standard: Transport Category Airplanes.” Federal Aviation Regulations
- Nacelle Selection Report, Lockheed LR 20963 Nov. 13 1967
- “Determination of Fuselage Cross-Section, Lockheed LR 21009 Oct. 16 1967
- Beach J. B. “Designing The Lockheed L-1011 to Meet Airline Needs beyond 1970.” SAE Transactions 77 paper 680545
- Model Specification, Lockheed LR 20111 March 1 1969
- “Basic Performance, Rolls-Royce RB.211-22-02 Engines,” Lockheed LR 21482 L-1011-385-1 March 5 1969
- “Introducing the Lockheed L-1011 to Its Flight Deck Crew,” Lockheed LR 21572 May 25 1968