Abstract: A cubesat communication system implementing addressable data packet for transmitting information collected by the cubesat to one or more receive-only ground stations. The cubesat may transmit information to the receive-only ground stations according to a scheduler. The receive-only ground stations may receive information from the cubesat without sending any commands to the cubesat to prompt transmission and re-transmit to a central common station using a bent pipe streaming protocol. Information between the cubesat and the ground station may be transmitted via a connectionless, datagram network protocol.

Abstract: Systems and methods are disclosed herein for adaptively coordinating among satellite communication channels.

Abstract: A cubesat communication system implementing addressable data packet for transmitting information collected by the cubesat to one or more receive-only ground stations. The cubesat may transmit information to the receive-only ground stations according to a scheduler. The receive-only ground stations may receive information from the cubesat without sending any commands to the cubesat to prompt transmission and re-transmit to a central common station using a bent pipe streaming protocol. Information between the cubesat and the ground station may be transmitted via a connectionless, datagram network protocol.

Abstract: A cubesat communication system implementing addressable data packet for transmitting information collected by the cubesat to one or more receive-only ground stations. The cubesat may transmit information to the receive-only ground stations according to a scheduler. The receive-only ground stations may receive information from the cubesat without sending any commands to the cubesat to prompt transmission and re-transmit to a central common station using a bent pipe streaming protocol. Information between the cubesat and the ground station may be transmitted via a connectionless, datagram network protocol.

Abstract: Systems and methods are disclosed herein for adaptively coordinating among satellite communication channels.

Abstract: Systems and methods are disclosed herein for adaptively coordinating among satellite communication channels.

Abstract: Systems and methods are disclosed herein for adaptively coordinating among satellite communication channels.

Abstract: A power distribution system and a method thereof regulate power distribution in a small form factor satellite flight system. The power distribution system may include a power source and a plurality of power channels. The power channels may distribute power from the power source to a plurality of systems in the small form factor satellite flight system. A processor may monitor power availability of the power source. The processor may also collect housekeeping information of the plurality of systems in the small form factor satellite flight system. The processor may regulate the power channels based on the power availability and the housekeeping information.

Abstract: A cubesat communications system includes an on-board computer implemented on a hardware platform. The on-board computer may include a system on module having a processor and a memory storing “boot” information. The on-board computer may also include a plurality of hardware interfaces implemented on the hardware platform to facilitate communication between the processor and a plurality of peripherals external to the on-board computer. The on-board computer may have a backplane having a plurality of connectors connecting the processor to the peripherals.

Abstract: A cubesat communication system implementing addressable data packet for transmitting information collected by the cubesat to one or more receive-only ground stations. The cubesat may transmit information to the receive-only ground stations according to a scheduler. The receive-only ground stations may receive information from the cubesat without sending any commands to the cubesat to prompt transmission and re-transmit to a central common station using a bent pipe streaming protocol. Information between the cubesat and the ground station may be transmitted via a connectionless, datagram network protocol.

Abstract: A back-plane connector connects component boards for a cubesat with a processing unit and a board connector electrically connected to the back-plane connector. The board connector mates with complimentary connectors on the component boards. The arrangement facilitates assembly, testing and operational reliability. An image capture system may be included and has an image capture device with a multiplexer for interactive collection and storage of image and video data.

Abstract: A back-plane connector connects component boards for a cubesat with a processing unit and a board connector electrically connected to the back-plane connector. The board connector mates with complimentary connectors on the component boards. The arrangement facilitates assembly, testing and operational reliability. An image capture system may be included and has an image capture device with a multiplexer for interactive collection and storage of image and video data.

Abstract: A cubesat communication system implementing addressable data packet for transmitting information collected by the cubesat to one or more receive-only ground stations. The cubesat may transmit information to the receive-only ground stations according to a scheduler. The receive-only ground stations may receive information from the cubesat without sending any commands to the cubesat to prompt transmission and re-transmit to a central common station using a bent pipe streaming protocol. Information between the cubesat and the ground station may be transmitted via a connectionless, datagram network protocol.

Abstract: A cubesat design includes selected subsystems for managing communications to other satellites and ground stations. In one embodiment, the subsystem includes a deployable antenna having compact size and low weight that reliably releases and detects an extended antenna after launch.

Abstract: A cubesat communications system includes an on-board computer implemented on a hardware platform. The on-board computer may include a system on module having a processor and a memory storing “boot” information. The on-board computer may also include a plurality of hardware interfaces implemented on the hardware platform to facilitate communication between the processor and a plurality of peripherals external to the on-board computer. The on-board computer may have a backplane having a plurality of connectors connecting the processor to the peripherals.

Abstract: A radio communications system and its method thereof handle radio communications for a small form factor satellite. The radio communications system may be implemented by a single printed circuit board. The single printed circuit board may include a UHF/VHF radio, an S-band radio and a processor. The processor may be coupled to the radios. The processor may receive radio messages from the UHF/VHF radio, and generate command signals based on the radio messages. The processor may transmit the command signals to a plurality of systems coupled to the radio communications system via a bus.

Abstract: A power distribution system and a method thereof regulate power distribution in a small form factor satellite flight system. The power distribution system may include a power source and a plurality of power channels. The power channels may distribute power from the power source to a plurality of systems in the small form factor satellite flight system. A processor may monitor power availability of the power source. The processor may also collect housekeeping information of the plurality of systems in the small form factor satellite flight system. The processor may regulate the power channels based on the power availability and the housekeeping information.

Abstract: A cubesat design includes selected subsystems for managing communications to other satellites and ground stations. In one embodiment, the subsystem includes a deployable antenna having compact size and low weight that reliably releases and detects an extended antenna after launch.

Abstract: A cubesat communication system implementing addressable data packet for transmitting information collected by the cubesat to one or more receive-only ground stations. The cubesat may transmit information to the receive-only ground stations according to a scheduler. The receive-only ground stations may receive information from the cubesat without sending any commands to the cubesat to prompt transmission and re-transmit to a central common station using a bent pipe streaming protocol. Information between the cubesat and the ground station may be transmitted via a connectionless, datagram network protocol.

Abstract: A back-plane connector connects component boards for a cubesat with a processing unit and a board connector electrically connected to the back-plane connector. The board connector mates with complimentary connectors on the component boards. The arrangement facilitates assembly, testing and operational reliability. An image capture system may be included and has an image capture device with a multiplexer for interactive collection and storage of image and video data.