Abstract: An orbital transfer vehicle system for cargo delivery is described herein. An orbital transfer vehicle (OTV) resides in space at a staging orbit. The OTV is configured for interfacing with a cargo pod at an insertion orbit to form a mated stack including the OTV and the cargo pod. The OTV is further configured for providing propulsion and rendezvous operations for transporting the mated stack to an intended target destination. Upon completion of delivery of the cargo pod to its intended target destination, the OTV then releases the cargo pod and returns to the staging orbit.

Abstract: An energy conversion and transmission system includes a thermal energy converter configured to convert thermal blackbody radiation energy to thermal infrared (IR) energy and to output a thermal IR energy stream. The system further includes a transmission device configured to receive the thermal IR energy stream from the thermal energy converter at a first location and output the thermal IR energy stream at a second location. The transmission device supplies the thermal IR energy stream to a thermal IR energy destination at the second location.

Abstract: Systems and methods of manufacture of radiator fins. In one embodiment, a radiator fin made of carbon fiber is provided. In one aspect, the radiator fin is made of carbon fibers forming an interlaced pattern. In another aspect, the interlaced carbon fiber radiator fin is attached directly to a heat pipe, the heat pipe connected to a heat source.

Abstract: A modular and scalable system to transfer space articles between space orbits. In one embodiment, the system employs a rendezvous vehicle which docks with a space article in an initial orbit, the connected stack then docking with a locomotive vehicle which maneuvers to a targeted orbit where the space article is detached. In one feature, the rendezvous vehicle and locomotive vehicle use a common propellant and the space article is a satellite.

Abstract: An energy conversion and transmission system includes a thermal energy converter configured to convert thermal blackbody radiation energy to thermal infrared (IR) energy and to output a thermal IR energy stream. The system further includes a transmission device configured to receive the thermal IR energy stream from the thermal energy converter at a first location and output the thermal IR energy stream at a second location. The transmission device supplies the thermal IR energy stream to a thermal IR energy destination at the second location.

Abstract: Systems and methods of manufacture of radiator fins. In one embodiment, a radiator fin made of carbon fiber is provided. In one aspect, the radiator fin is made of carbon fibers forming an interlaced pattern. In another aspect, the interlaced carbon fiber radiator fin is attached directly to a heat pipe, the heat pipe connected to a heat source.

Abstract: A modular and scalable system to transfer space articles between space orbits. In one embodiment, the system employs a rendezvous vehicle which docks with a space article in an initial orbit, the connected stack then docking with a locomotive vehicle which maneuvers to a targeted orbit where the space article is detached. In one feature, the rendezvous vehicle and locomotive vehicle use a common propellant and the space article is a satellite.