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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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Top View
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
Technology for NASA Large Space Systems
Spacecraft Early Design Validation Using Formal Methods
Acute Radiation Risk and BRYNTRN Organ Dose Projection)
Advanced Spacecraft Technology Program
High Performance Optical Imaging Payloads for Smallsat Missions
Overview of the NPS Spacecraft Architecture and Technology Demonstration Satellite, NPSAT1
Spacecraft Design Guidelines
Orion Spacecraft Includes Both Crew and Service ORION Attitude Control Motor CREW EXPLORATION VEHICLE
Spacecraft Design Optimisation for Demise and Survivability
Space Systems Engineering
Towards More Effective Teaching Strategies of Iteration and Systems Management in Spacecraft De- Sign
A Reliability Engineering Approach for Managing Risks in Cubesats
The Chipsat Spacecraft Design – Significant Science on a Low Budget
On-Orbit Satellite Servicing Study Project Report / NASA
An Overview of the Mission Design Process.The NASA Engineering Management Council
Integrating Reliability Engineering with Fault Management to Create Resilient Space Systems
Safety-Guided Spacecraft Design Using Model
Master's Thesis
Integrated Transportation System Design Optimization Christine
GAO-13-276SP, NASA: Assessments of Selected Large-Scale Projects
Mission to Mars Vehicle Concept and Design
Download Full Text (Pdf)
Guidelines and Capabilities for Designing Human Missions
AU-18 Space Primer
A Suborbital Spaceship for Short Duration Space and Microsat Launch Pat Bahn TGV Rockets 1928 Goddard Drive, Norman OK 73069
[email protected]
, +1.405.366.0779
Spacecraft Instrumentation: Integrating Design Across the Curriculum
Spacecraft Structures
Preliminary System Development and Detailed Structural Design and Analysis for the Canx-7 Nanosatellite
Spacecraft Design FRS 148, Princeton University Robert Stengel
Human Integration Design Processes (HIDP) Human Health and Performance Directorate
Optical Communications Development for Spacecraft Applications
A Systematic Process for Assessing Human Spacecraft Designs in Terms of Relative Safety and Operational Characteristics
Design and Implementation of Eps (Electrical Power System) of a Cubesat
Systems Engineering and Spacecraft Subsystems Modeling As Prerequisites for Capstone Design
ICES-2020-150.Pdf (443.5Kb)
Estimating the Reliability of Electronic Parts in High Radiation Fields
Methods for Analysis of Preliminary Spacecraft Designs AAE450, Spacecraft Design, Purdue University