Sizing and Margins Assessment of Mars Science Laboratory Aeroshell Thermal Protection System
Development of the Mars Science Laboratory Heatshield Thermal Protection System
U.S. SPACESUIT LEGACY: MAINTAINING IT FOR THE FUTURE
CONCEPTUAL DESIGN OF A NEXT GENERATION, 150 PASSENGER COMMERCIAL TRANSPORT
Modeling of Stardust Entry at High Altitude, Part 1: Flowfield Analysis
Impact of Using Reliever Airports to Absorb Additional Demand in the Potomac TRACON
Ground-to-Flight Traceability Analysis of Arcjet Testing for the Crew Exploration Vehicle
The Effect of Future Vehicles on Controller and Pilot Workload