Additional Design Studies of the NASA/Navy Lift/Cruise Fan
Rationalization of Power Subsystem Design Specifications for ESA Spacecraft
Review of Air Force's Next Generation Trainer Aircraft Program Department of Defense
Orbital Transfer Vehicle Launch Operations Study. Volume 2. Detailed Summary
Preliminary Design of a Family of Three Close Air Support Aircraft
Two-Stage Reusable Launch System Utilizing a Winged Core Vehicle and Glideback Boosters