Lockheed Martin Corporation

Road-iq, LLC

Rory Nell McLeod

Mark M Moeller

Lester Meeks

Darren Andrew Kearney

Collin J Topolski

Ryan Earl Roberts

Joseph Paul Arves

Peter John Whitehead

Jeffery Robert Porter

Ilko Dossev

Herbert Stephen Jones

Herbert Stephens Jones

Disclosed herein, in one example, is a device for aggregating networks and serving data from those networks to computers for integrating information from various systems in a vehicle, processing that information, and presenting it to consumers of information in a suitable format. The device for aggregating networks, in another example, is specific to a vehicle and serving data from those networks to computers. The device, in one example, generally includes three main pieces: a motherboard containing the electronics embodying the vehicle computer system; software which implements the instructions for the electronics enabling the functionality disclosed herein; and, a case to protect the motherboard and provide a method of mounting the devices.

Device and system for aggregating networks and serving data from those networks to computers

Disclosed herein, in one example, is a device for aggregating networks in a vehicle and serving data, including video data, from those networks to a computer for integrating information from various systems in a vehicle, processing that information, and presenting the information to a user in a suitable format. The device for aggregating networks, in another example, is specific to a vehicle and serving data, including video data, from those networks to computers.

Device, system and method for aggregating networks and serving data from those networks to computers

A rocket engine ( ) generates a flow of hot propulsion fluid through a nozzle ( N) for generating propulsive thrust along a thrust vector Hybrid exhaust gas generators ( ) have their exhausts ( ) through the side of the nozzle. Each gas generator includes a fuel grain ( ) and a source of oxidizer ( ). The fuel grain is kept hot by either or both (a) direct radiation or conduction from the hot propulsion fluid, or (b) by a trickle of oxidizer. The fuel grain can thus react quickly to a substantial flow of oxidizer.

Hybrid injection thrust vector control

A rocket engine ( ) generates a flow of hot propulsion fluid through a nozzle ( N). Hybrid exhaust gas generators ( ) have their exhausts ( ) through the side of the nozzle. Each gas generator includes a fuel grain ( ) and a source of oxidizer ( ). The fuel grain is kept hot by either or both (a) direct radiation or conduction from the hot propulsion fluid, or (b) by a trickle of oxidizer. When the thrust vector is to be modified, the appropriate one of the hybrid gas generators receives a flow of oxidizer, and the resulting exhaust gas is injected through the side of the nozzle.

Growing community of inventors

Lynden, WA, United States of America

Rory Nell McLeod