Moog Space Vehicles are designed to launch on VCLV and NSSL-class launch vehicles (Atlas V, Vulcan, Falcon 9) while supporting up to 1,500 kg of secondary payloads with a variety of standard separation systems. They can be used to disperse small satellite constellations, act as a Hosted Payload platform, or deliver a single spacecraft to its ideal orbit. They are modular platforms and have their own avionics, power, propulsion, and communications systems that are configurable for short durations up through multiyear missions in a wide range of orbits and transfer capabilities. Green propellant propulsion systems in the smaller platforms and traditional storable hydrazine propellant in the larger platforms provide the capability for several different missions, including deploying small spacecraft in multiple orbits.