Add to ORKGThe aircraft development program, budgetary estimates in CY 1976 dollars, and cost reduction program variants are presented. Detailed cost matrices are also provided for the mechanical transmission system, turbotip transmission system, and the thrust vector hoods and yaw doors
Definitions of takeoff gross weight, performance, and direct operating cost for both a 30 and 50 pas...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
An assessment of risk, in terms of delivery delays, cost overrun, and performance achievement, assoc...
Concept design is presented for two types of lift/cruise fan technology V/STOL aircraft, turbotip fa...
Two types of lift/cruise fan technology aircraft were conceptually designed. One aircraft used turbo...
Assessed are the risks associated with the lift/cruise fan technology V/STOL aircraft program. Three...
Technology flight vehicles were defined for three different approaches which demonstrate the concept...
A three engine, three fan V/STOL airplane was designed for use as a Research Technology Airplane in ...
A conceptual design analysis is performed on a single engine V/STOL supersonic fighter/attack concep...
In anticipation of an eventual VTOL requirement for civil aviation, NASA has been conducting studies...
Wind tunnel test support, aircraft contractor support, a propulsion system computer card deck, preli...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
The V/STOL Research and Technology Aircraft (RTA)propulsion system design effort is limited to compo...
The economic aspects of the STOL aircraft for short-haul air transportation are discussed. The study...
A study program for conceptual design studies of remote lift and lift/cruise fan systems to meet the...
Definitions of takeoff gross weight, performance, and direct operating cost for both a 30 and 50 pas...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
An assessment of risk, in terms of delivery delays, cost overrun, and performance achievement, assoc...
Concept design is presented for two types of lift/cruise fan technology V/STOL aircraft, turbotip fa...
Two types of lift/cruise fan technology aircraft were conceptually designed. One aircraft used turbo...
Assessed are the risks associated with the lift/cruise fan technology V/STOL aircraft program. Three...
Technology flight vehicles were defined for three different approaches which demonstrate the concept...
A three engine, three fan V/STOL airplane was designed for use as a Research Technology Airplane in ...
A conceptual design analysis is performed on a single engine V/STOL supersonic fighter/attack concep...
In anticipation of an eventual VTOL requirement for civil aviation, NASA has been conducting studies...
Wind tunnel test support, aircraft contractor support, a propulsion system computer card deck, preli...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
The V/STOL Research and Technology Aircraft (RTA)propulsion system design effort is limited to compo...
The economic aspects of the STOL aircraft for short-haul air transportation are discussed. The study...
A study program for conceptual design studies of remote lift and lift/cruise fan systems to meet the...
Definitions of takeoff gross weight, performance, and direct operating cost for both a 30 and 50 pas...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
An assessment of risk, in terms of delivery delays, cost overrun, and performance achievement, assoc...