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Spacecraft design

A Quantitative Human Spacecraft Design Evaluation Model For
An Integrated Reliability and Physics-Based Risk Modeling Approach for Assessing Human Spaceflight Systems
Spacecraft Research and Design
Design Standard Spacecraft Charging and Discharging
Spacecraft Design Innovations in the Apl Space Department
Design and Utilization of the Stanford Vision-Based Navigation Testbed for Spacecraft Rendezvous
Arxiv:1906.05079V1 [Astro-Ph.IM] 12 Jun 2019
Integrating Spacecraft Systems
System Engineering of Photonic Systems for Space Application
JERG-2-000 Spacecraft Design Standard
The Spacecraft Design/Flight Experience at the Undergraduate Level
Failures in Spacecraft Systems: an Analysis from The
Small Satellite Solutions with Large Satellite Implications
Affordable Spacecraft: Design and Launch Alternatives (Part 7 of 8)
Reliability, Multi-State Failures and Survivability of Spacecraft and Space-Based Networks
Xenia Mission: Spacecraft Design Concept
Final Report System Design of the Pioneer Venus Spacecraft
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Design, Implementation, and Analysis of Electrical System Architecture for Cubesat to Ground Communications
Modeling Uncertainties of Spacecraft Design Parameters for Cost-Risk Analysis
A Reliability Model for the Design and Optimization of • Separated Spacecraft Interferometer Arrays Cyrus D
A Total Systems Analysis Method for the Conceptual Design of Spacecraft: an Application to Remote Sensing Imager Systems
LSIC Spring Meeting Program.Pdf
The System Approach to Successful Space Mission Development
A Reference Architecture for Cubesat Development
AFFORDABLE SPACECRAFT: Design and Launch Alternatives
Guide Space Plug-And-Play Architecture Standards
The Venus Express Spacecraft System Design
First Century Commercial Space Imperative
Ssc19-Wkiv-08
The Exploring Machines. National Aeronautics and Space Administra
1 Spacecraft Systems Design
An Inquiry of Space Architecture: Design Considerations and Design Process
(Smaf) Handbook for Uncrewed Space Missions
Automating the Process of Optimization in Spacecraft Design
THEMIS Post Launch Spacecraft Bus Systems Performance Validation: Comparison to Systems Design and Analysis Attributes

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