This paper presents a design of a military transport aircraft capable of carrying 800,000 lbs of payload from any point in the United States to any other point in the world. Such massive airlift requires aggressive use of advanced technology and a unique configuration. The Cetaceopteyx features a joined wing, canard and six turbofan engines. The aircraft has a cost 1.07 billion (1993) dollars each. This paper presents in detail the mission description, preliminary sizing, aircraft configuration, wing design, fuselage design, empennage design, propulsion system, landing gear design, structures, drag, stability and control, systems layout, and cost analysis of the aircraft
A propulsion-controlled aircraft (PCA) system for emergency flight control of aircraft with no fligh...
The purpose of this project is to provide an empennage structural assembly that will withstand the o...
This report presents work carried out under contract DE-AC22-95PC95144 ''Combustion 2000 - Phase II....
A millimeter-wave TWT was developed using a dispersive, high-impedance forward wave interaction stru...
Planned payload crew utilization on Spacelab mission are analyzed to establish trends and guidelines...
Mechanical Engineering Senior Design Project 1 (ME4182) is a part of the NASA/University Advanced De...
This report analyzes and presents a preliminary design for an experimental hypersonic vehicle. This ...
The tethered satellite system (TSS) was envisioned as a means of extending a satellite from its base...
The cryogenic/aerobrake (CAB) and the cryogenic all-propulsive (CAP) concept designs developed in su...
The zero-gravity environment creates a need for a proper human body restraint system to maintain a c...
A series of flight tests was conducted to evaluate the reduction of takeoff ground roll distance obt...
The TATSS Project's goal was to develop a design for computer software that would support the attain...
The results of a consulting effort to aid NASA Ames-Dryden in defining a new initiative in aircraft ...
A heat pump is a device which elevates the temperature of a heat flow by a means of an energy input....
Slow-moving vehicles are commonly found on the rural roads of Iowa. Common slow-moving vehicles in I...
A propulsion-controlled aircraft (PCA) system for emergency flight control of aircraft with no fligh...
The purpose of this project is to provide an empennage structural assembly that will withstand the o...
This report presents work carried out under contract DE-AC22-95PC95144 ''Combustion 2000 - Phase II....
A millimeter-wave TWT was developed using a dispersive, high-impedance forward wave interaction stru...
Planned payload crew utilization on Spacelab mission are analyzed to establish trends and guidelines...
Mechanical Engineering Senior Design Project 1 (ME4182) is a part of the NASA/University Advanced De...
This report analyzes and presents a preliminary design for an experimental hypersonic vehicle. This ...
The tethered satellite system (TSS) was envisioned as a means of extending a satellite from its base...
The cryogenic/aerobrake (CAB) and the cryogenic all-propulsive (CAP) concept designs developed in su...
The zero-gravity environment creates a need for a proper human body restraint system to maintain a c...
A series of flight tests was conducted to evaluate the reduction of takeoff ground roll distance obt...
The TATSS Project's goal was to develop a design for computer software that would support the attain...
The results of a consulting effort to aid NASA Ames-Dryden in defining a new initiative in aircraft ...
A heat pump is a device which elevates the temperature of a heat flow by a means of an energy input....
Slow-moving vehicles are commonly found on the rural roads of Iowa. Common slow-moving vehicles in I...
A propulsion-controlled aircraft (PCA) system for emergency flight control of aircraft with no fligh...
The purpose of this project is to provide an empennage structural assembly that will withstand the o...
This report presents work carried out under contract DE-AC22-95PC95144 ''Combustion 2000 - Phase II....