Advanced Design Project

TADP Candidate Projects

Mars Sample Return Cannister Solar Electric Propulsion Spacecraft
Mars Ascent Vehicles Lunar Communications System
Logistics Modules for Gateway Resupply Lunar and Mars Surface Mobibilty
Parametric Sizing Routines System Simulation Tools
Space Shuttle Crew Escape Inflatable Aeroshells
Electronic Archives Mars Mission Module
Deep Space Mission Electric Propulsion Test Facility
Thrust Measurement Device Large Space Power Generator
PEM Fuel Cell Instrumentation DC to DC Converter Evaluation
Distributed Architecture - Multiple Projects
All Candidate Projects

If you have any questions concerning this project, please contact the Project Coordinator, Michelle Matanic.


Last Modified: August 17, 2001