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title: Journal of spacecraft and rockets
Qualitative Assessment of Aerocapture and Applications to Future Missions
Feasibility and Performance of Atmospheric-Breathing Propulsion for Mars Descent
Analysis was performed to assess the impact of atmospheric-breathing supersonic retropropulsion as a technology solution for Mars
...Mission Design and Performance Analysis of a Smallsat Aerocapture Flight Test
The co-delivery of a direct-entry probe and an aerocapture orbiter from a single atmospheric entry state is a novel way to include ride
...Inverse Estimation of the Mars Science Laboratory Entry Aeroheating and Heatshield Response
Optimal Information Filtering for Robust Aerocapture Trajectory Generation and Guidance
Entry flight is a critical mission phase of planetary aeroassist problems. During atmospheric flight, aleatory-epistemic uncertainty and
...Reconstruction of Mars Pathfinder Aeroheating and Heat Shield Response Using Inverse Methods
The Mars Pathfinder probe entered the Martian atmosphere in 1997 and contained instrumentation that provided measurements of the
...Comparison of Statistical Estimation Techniques for Mars Entry, Descent, and Landing Reconstruction
A Conceptual Modeling Approach for Performance of Magnetohydrodynamic Drag During Planetary Entry
Three-Dimensional Finite Element Ablative Thermal Response and Design of Thermal Protection Systems
A finite element ablation and thermal response program for the simulation of three-dimensional transient thermostructural analysis has
...Statistical Entry, Descent, and Landing Performance Reconstruction of the Mars Science Laboratory
Constitutive Model of Fiber Substrate Ablators for Conceptual Design
High-Altitude Divert Architecture for Future Robotic and Human Mars Missions
Numerical Methodology for the Conceptual Design of Conformal Ablative Heat Shields
Analytic Free-Molecular Aerodynamics for Rapid Propagation of Resident Space Objects
Conceptual Design of a Small Earth Reentry Vehicle for Biological Sample Return
Survey of Blunt-Body Supersonic Dynamic Stability
Computational Aerodynamic Predictions of Supersonic Retropropulsion Flowfields