SIERRA SPACE ECLIPSE Trademark

Satellite structural components, namely, satellite bus components in the nature of electrical harnesses, printed circuit boards (PCBs), electrical control panels featuring power distribution units, voltage regulators and monitoring devices for management and distribution of electrical power to satellite bus communication, propulsion and thermal control subsystems and integrated payloads; Satellite bus operational components for satellite power, propulsion, communication, attitude and orbit control (AOC), thermal control, telemetry, data and handling and for control and operation of integrated payload, namely, batteries, voltage regulators, microcontrollers, capacitors, relays, solar arrays, magnetometers, star trackers, telemetry transmitters, and on-board computers; recorded and downloadable software for powering and controlling satellites and for communication from and to satellites; Spacecraft operational subsystems comprised of solar array and antenna deployment mechanisms, radiators, radiator panels, payload and subsystem mounts, structural integration and propulsion mounting structures, deployment arms and supports

Manufacturing for others in the field of space operations, namely, manufacturing spacecraft structural components and satellite platforms; Manufacturing of structural components and operational subsystems of spacecraft for others; Custom manufacturing of spacecraft structural components to the specification of others, namely, building structural and operational components of a satellite bus for integration of customer payload; Manufacture of general product lines, namely, spacecraft components and satellite buses to the order and specification of others

Technical and engineering services in the field of spacecraft, namely, environmental and system testing of payloads with satellite buses to ensure satellite and payload work together and function as intended in space; Satellite payload integration services, namely, engineering design, testing and integration of payload and payload subsystems with satellite buses to ensure satellite and payload work together and function as intended in space; Environmental testing for compatibility with satellite buses and payloads; Operational and payload integration testing for satellite buses

Spacecraft, namely, satellite buses; Full line of satellite buses; Structural components for spacecraft, namely, frames, sub-frames, protective covers and shields, body panels, engine mounts, mounting brackets adapted for use with spacecraft, struts; Satellite buses and the structural and operational hardware and recorded software for satellite buses sold as a unit; Satellite components, namely, satellite buses, satellite support structures, and satellite apparatuses and recorded software for providing power, commands, telemetry, communication, radiation shielding, and attitude control sold as unit; structural insulated panels embedded with electronics for placement on satellites