Lessons Learned from the Long Duration Exposure Facility
Modifications of a Large Space Simulator for Cost Effective Testing
Testing in Combined Dynamic Environments
An Approach to Reduce Spacecraft Thermal Vacuum Test Timeline
Hold Down/Release Cylinder Acceptance Testing
Pyroshock Simulation for Satellite Components Using A Tunable Resonant Fixture
Automated Process for Notched Sine Testing
Quantifying the Factors that Affect Launch Vehicle Reliability and Operability
Using a Readiness Program to Increase the Efficiency of Spacecraft Integration and Test Programs
Research on the Structural Dynamics Verification of Flexible Spacecraft
Mars Observer System Thermal Vacuum Test and Its Cost Saving Approach
Orbital Debris Impact on a Simple Whipple Bumper Shield
Latest Program Developments in Europe and Related Test Aspects
The Evolution of a Test System/A Continuous Improvement Model
Verification Approach for Mini Pressurized Logistic Module of Space Station Freedom
High Data Rate Telemetry System
Force Limited Vibration Testing at JPL