THE TURBO-ELECTRIC VTOL AIRCRAFT, SUPPLEMENTAL INFORMATION

THE TURBO-ELECTRIC VTOL AIRCRAFT, SUPPLEMENTAL INFORMATION

In TG-1013 (AD-675 332) a unique aircraft propulsive/lift power distribution system was described that promises a great deal of flexibility in the design of VTOL aircraft. Its use would permit a significant improvement in many aspects of present and future VTOL designs, including performance, safety...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: Rabenhorst,David W
Format: Report
Sprache:eng
Schlagworte:
AEROSPACE SYSTEMS
DISTRIBUTION
DUCTED FANS
Electric and Ion Propulsion
ELECTRIC PROPULSION
ESCAPE SYSTEMS
GAS TURBINES
Jet and Gas Turbine Engines
LIFT
POWER
RECOVERY
SELF MANEUVERING UNITS
V/STOL
VERTICAL TAKEOFF AIRCRAFT
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Beschreibung
Zusammenfassung:In TG-1013 (AD-675 332) a unique aircraft propulsive/lift power distribution system was described that promises a great deal of flexibility in the design of VTOL aircraft. Its use would permit a significant improvement in many aspects of present and future VTOL designs, including performance, safety, cost, operability, noise, applicability, and operational economy. In this supplement (TG-1013A), a number of interesting additional Turbo-Electric applications that have been evolved since the publication of TG-1013 are described. (Author)