Extending Satellite Lifetimes in Geosynchronous Orbit with Servicing
Development of an Electrical Data Exchange Interface based on STEP AP212
ON-ORBIT SERVICING OF DEPARTMENT OF DEFENSE AND NATIONAL SECURITY SPACE ASSETS
Particle acceleration, magnetic field generation, and emission in relativistic shocks
Particle acceleration, magnetic field generation, and emission in relativistic shocks
Development of an electrical data exchange interface based on STEP AP212
Large Eddy Simulation of a Harrier Aircraft at Touch Down
NigeriaSat-2 AOCS: Results from the First 90 Days in Orbit (AAS 12-093)
Enhancing NSS System Engineering Analysis through Value-Centric Design Methodology
Enhancing NSS System Performance by Including Value-Centric Analysis (VCA)
Small satellite computer-aided design and manufacturing
A General Methodology for Analysis of Structure-Borne Micro-Vibration
Low Cost Propulsion Developments for Small Spacecraft at the Surrey Space Centre
Energy Dissipation in Spacecraft Structures Incorporating Bolted Joints Operating in Macroslip