The results of four years research on technology are synthesized in an advanced supersonic cruise aircraft design. Comparisons are presented with the former United States SST and the British-French Concorde, including aerodynamic efficiency, propulsion efficiency, weight efficiency, and community noise. Selected trade study results are presented on the subjects of design cruise Mach number, engine cycle selection, and noise suppression. The critical issue of program timing is addressed and some observations made regarding the impact that timing has on engine selection and minimization of program risk
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
Engine performance and mission studies were carried out for a single-spool Turbine Bypass Engine con...
The objective was to compare the characteristics of SSTs designed for the same mission by Lockheed, ...
Research and development programs provide confidence that technology is in-hand to design an economi...
The need for greatly improved fuel efficiency and off-design subsonic characteristics is discussed. ...
The impact of advanced supersonic technologies on the performance and characteristics of a supersoni...
An analytical study of a supersonic-cruise, executive, jet aircraft indicated the effects of using a...
The effects of possible increases in cruise speed over present-day transport aircraft were investiga...
Technical progress made in each of the disciplinary research areas affecting the design of supersoni...
Technology assessment studies were conducted to provide an updated technology base from which an adv...
Sustained supersonic cruise propulsion systems for military applications are studied. The J79-5 in t...
For several years there was a growing interest in the subject of efficient sustained supersonic crui...
NASA computer codes in the areas of preliminary sizing and enroute performance, takeoff and landing ...
System and design integration studies are presented to define and assess the application of the adva...
A study was made to examine the effect of advanced technology engines on the performance of subsonic...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
Engine performance and mission studies were carried out for a single-spool Turbine Bypass Engine con...
The objective was to compare the characteristics of SSTs designed for the same mission by Lockheed, ...
Research and development programs provide confidence that technology is in-hand to design an economi...
The need for greatly improved fuel efficiency and off-design subsonic characteristics is discussed. ...
The impact of advanced supersonic technologies on the performance and characteristics of a supersoni...
An analytical study of a supersonic-cruise, executive, jet aircraft indicated the effects of using a...
The effects of possible increases in cruise speed over present-day transport aircraft were investiga...
Technical progress made in each of the disciplinary research areas affecting the design of supersoni...
Technology assessment studies were conducted to provide an updated technology base from which an adv...
Sustained supersonic cruise propulsion systems for military applications are studied. The J79-5 in t...
For several years there was a growing interest in the subject of efficient sustained supersonic crui...
NASA computer codes in the areas of preliminary sizing and enroute performance, takeoff and landing ...
System and design integration studies are presented to define and assess the application of the adva...
A study was made to examine the effect of advanced technology engines on the performance of subsonic...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
Engine performance and mission studies were carried out for a single-spool Turbine Bypass Engine con...
The objective was to compare the characteristics of SSTs designed for the same mission by Lockheed, ...