Technology for Small Spacecraft
Robust and Safe -Spacecraft Swarming in Perturbed Near-Circular Orbits
Cubesat Asteroid Mission: Propulsion Trade-offs
Advanced Dual-Pull Mechanism for Deployable Spacecraft Booms
Space Launch System: SLS at Critical Design Review
Research of design of a small spacecraft with an electrothermal propulsion system
Applications of a Single-Vector Inertial Aiding Scheme for 3U CubeSats
Nutational Stability of a Dual-Spin Satellite under the Influence of Applied Reaction Torques
Geolocation of Formation-Flying Spacecraft Using Relative Position Vector Measurements
Optical Communications for NASA's Small Spacecraft Missions of the Future
Consider-Filter-Based On-Orbit Coarse Sun Sensor Calibration Sensitivity
Spacecraft Thermal Control Management Using Electrochromics
Government-owned CubeSat Next Generation Bus Reference Architecture
Real-Time Nonlinear Attitude Control System for Nanosatellite Applications
Attitude Control of a Small Spacecraft via Tube-Based Model Predictive Control
Adaptive Momentum Distribution Jitter Control for Microsatellite
Spacecraft Formation Flying Dynamics and Control Using the Geomagnetic Lorentz Force
Sun Vector–Based Attitude Determination of Passively Magnetically Stabilized Spacecraft
Embracing Innovation in Aviation While Respecting Its Safety Tradition
Real-Time Attitude-Independent Magnetometer Bias Estimation for Spinning Spacecraft
TechEdSat - An Educational 1U CubeSat Architecture Using Plug-and-Play Avionics
Impact of Atmospheric Coupling Between Orbit and Attitude in Relative Dynamics Observability
Optical Communications and Sensor Demonstration
Application of Low-Power Pulse Plasma Thrusters in Thrust Units of Small Spacecrafts
Decision Analysis Tool for Small Satellite Risk Management
Sounding rocket SS-520 as a CubeSat launch vehicle
The Standardized Functional Support Sectional for the Small Astronomy Satellite (Sas)
Adaptive Singularity-Free Control Moment Gyroscopes
NanoSat Constellation Mission Design
Three Hundred Fifty Volt Photovoltaic Power Generation in Low Earth Orbit
Review of NASA Ames CubeSat Program
Basic Design Considerations for a Small Scientific Satellite
System Definition Phase and Acquisition Phase Project Plan for Small Astronomy Satellite Sas-D
Commercial Space Industry Launches a New Phase
Green Monopropellant Status at Marshall Space Flight Center
Recoverable Capsules on Ariane
Whole-Spacecraft Vibration Isolation on Small Launch Vehicles
Reference Architecture for CubeSat Development
Flight Demonstration of Autonomous Noncooperative Rendezvous in Low Earth Orbit
Small Explorer Data System MIL-STD-1773 Fiber Optic Bus
Optimal Spacecraft Attitude Control