Approach And Landing Investigation At Lift Drag Ratios Of 2 To 4 Utilizing A Straight Wing Fighter Airplane
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Wingless Flight
Author | : R. Dale Reed |
Publisher | : University Press of Kentucky |
Total Pages | : 404 |
Release | : 2021-10-21 |
Genre | : Technology & Engineering |
ISBN | : 0813185637 |
Most lifting bodies, or "flying bathtubs" as they were called, were so ugly only an engineer could love them, and yet, what an elegant way to keep wings from burning off in supersonic flight between earth and orbit. Working in their spare time (because they couldn't initially get official permission), Dale Reed and his team of engineers demonstrated the potential of the design that led to the Space Shuttle. Wingless Flight takes us behind the scenes with just the right blend of technical information and fascinating detail (the crash of M2-F2 found new life as the opening credit for TV's "The Six Million Dollar Man"). The flying bathtub, itself, is finding new life as the proposed escape-pod for the Space Station.
Scientific and Technical Aerospace Reports
Author | : |
Publisher | : |
Total Pages | : 1004 |
Release | : 1976 |
Genre | : Aeronautics |
ISBN | : |
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Low-lift-to-drag-ratio Approach and Landing Studies Using a CV-990 Airplane
Author | : Berwin M. Kock |
Publisher | : |
Total Pages | : 52 |
Release | : 1972 |
Genre | : Space shuttles |
ISBN | : |
Results are presented of a flight-test program utilizing a CV-990 airplane, flow in low-lift-to-drag-ratio (L/D) configurations, to simulate terminal area operation, approach, and landing of large unpowered vehicles. The results indicate that unpowered approaches and landings are practical with vehicles of the size and performance characteristics of the proposed shuttle vehicle. Low L/D landings provided touchdown dispersion patterns acceptable for operation on runways of reasonable length. The dispersion pattern was reduced when guidance was used during the final approach. High levels of pilot proficiency were not required for acceptable performance.--P. [i].
The Stabilizing Effectiveness of Conical Flares on Bodies with Conical Noses
Author | : Donn B. Kirk |
Publisher | : |
Total Pages | : 54 |
Release | : 1959 |
Genre | : Aerodynamic load |
ISBN | : |