Single Particle Damage Events in Candidate Star Camera Sensors (AAS 05-074)
Precision Orbit Determination for the Mars Observer Mission (AAS 93-602)
Precision Orbit Determination and Gravity Field Improvement Derived from TDRSS
Precise Orbit Determination for the TOPEX/Poseidon Mission (AAS 93-577)
Engine Exhaust Emissions Evaluation of a Cummins L10E When Fueled with a Biodiesel Blend
Development of Insensitive Rocket Propellants Based on Ammonium Nitrate and Polynimmo
Conservative Force Model Performance for TOPEX/Poseidon Precision Orbit Determination (AAS 93-268)
An Assessment of TDRSS for Precision Orbit Determination
2005-01-1857 A NOx Reduction Solution for Retrofit Applications: A Simple Urea SCR Technology