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Launch Systems | Space Systems | Mission Engineering

XNAV for Deep Space Navigation

Abstract: The concept of utilizing pulsars for spacecraft navigation has been in development since the discovery of these rapidly rotating neutron stars in the 1960’s [1]. The Jet Propulsion Laboratory (JPL) conducted studies in the 70’s and 80’s proposing the use of...

Plug-and-Play for Creating “Instant” GN&C Solutions

Abstract: Small satellites provide an excellent, near-term platform for demonstrating a responsive capability highlighting missions that necessitate quick launch, quick operational capability, with an attendant, very short development schedule. To achieve this rapid...

Circular vs. Elliptical Orbits for Persistent Communications

Abstract: Responsive Communications missions typically require “persistent communications,” i.e., repeat coverage that lasts for an extended period or the entire day. LEO orbits cannot provide this coverage without a large number of satellites and GEO satellites are...

Systems Engineering for Responsive Launch

Abstract: In the Microcosm Responsive Launch Systems model, a key requirement is that the launch vehicle be essentially a commodity, built to inventory, and ready to go whenever needed, much like cruise missiles or rental cars. This, in turn, implies the need for low...