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Mars atmospheric entry
MARS SCIENCE LABORATORY ORBIT DETERMINATION Gerhard L. Kruizinga(1)
IMU/MCAV Integrated Navigation for the Powered Descent Phase Of
Space Vehicle Conceptual Design Blue Team March 20, 2021
Development of Supersonic Retropropulsion for Future Mars Entry, Descent, and Landing Systems
Co-Optimization of Mid Lift to Drag Vehicle Concepts for Mars Atmospheric Entry
The Exomars Programme
2018 Mars Insight Mission Design and Navigation Overview
Human Exploration of Mars: the Reference Mission of the NASA
Human Exploration of Mars Design Reference Architecture 5.0
Mars Science Laboratory Launch
Mars 2020 Mission Design and Navigation Overview Aas 19
Supersonic Retro Propulsion Flight Vehicle Engineering of a Human Mission to Mars
Mars Xpress Summary of the Group Design Project Msc in Astronautics and Space Engineering 1997/98 Cranfield University
Low Density Supersonic Decelerators
Mission Design and Navigation Analysis of the Esa Exomars Program
2018 Mars Insight Trajectory Reconstruction and Performance from Launch Through Landing
A Study on Mars Probe Failures
MARSWRF Prediction of Entry Descent Landing Profiles
Top View
Mars Aerocapture Systems Study
Mars Phoenix Entry, Descent, and Landing Simulation De- Sign and Modelling Analysis
Design and Optimization of Navigation and Guidance Techniques for Mars Pinpoint Landing: Review and Prospect Zhengshi Yu1,2, Pingyuan Cui*1,2, John L
From the Martian Surface to Its Low Orbit in a Reusable Single-Stage Vehicle—Charon
Guidance and Control Algorithms for the Mars Entry, Descent and Landing Systems Analysis
Mars 2018 MAX-C Caching Rover
Human Mars Exploration and Expedition Challenges
[Paper Number]
Robust Mars Atmospheric Entry Integrated Navigation Based on Parameter Sensitivity
IAA-AAS-Scitech2020-019 ORBITAL and PLANETARY CHALLENGES
Effects of Water Vapor Presence in Martian Atmospheric Entry Plasma
Mars Science Laboratory
2016 Mars Insight Mission Design and Navigation
Guidance of Reusable Launchers: Improving Descent and Landing Performance
Guidance and Control for Mars Atmospheric Entry: Adaptivity and Robustness 1
Precision Guidance for Mars Entry with a Supersonic Inflatable Aerodynamic Decelerator
Keep Mars Clean: the Need for Space Policy to Avoid Planetary Space Debris
Radio/FADS/IMU Integrated Navigation for Mars Entry
Mission Overview ===The Mars
Mars Base Camp Updates and New Concepts
Space Exploration & Space Colonization Handbook