Organizational Unit:
Space Systems Design Laboratory (SSDL)
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Publication Search Results
Exploring the F6 Fractionated Spacecraft Trade Space with GT-FAST
Response Surface Equations for Expendable Launch Vehicle Payload Capability
Fast Sensitivity Computations for Trajectory Optimization
Performance Characterization of Supersonic Retropropulsion for Application to High-Mass Mars Entry, Descent, and Landing
Comparative Reliability of GEO, LEO, and MEO Satellites
High Mass Mars Entry, Descent, and Landing Architecture Assessment
Trading Robustness Requirements in Mars Entry Trajectory Design
Statistical Reliability Analysis of Satellites by Mass Category: Does Spacecraft Size Matter?
GT-FAST: A Point Design Tool for Rapid Fractionated Spacecraft Sizing and Synthesis
Angle of Attack Modulation for Mars Entry Terminal State Optimization