Abstract: Pivot mechanisms for tracking cameras are disclosed herein. A tracking camera assembly includes a camera head having a housing and a pivot joint disposed within the housing. The pivot joint fitting is configured to rotate with respect to the housing. A cable is in electrical communication with the camera head and is fixedly coupled to the pivot joint fitting and extends away from the camera head. A stand pole is fixedly coupled to the pivot joint fitting and extends away from the camera head.

Abstract: Pivot mechanisms for tracking cameras are disclosed herein. A tracking camera assembly includes a camera head having a housing and a pivot joint disposed within the housing. The pivot joint fitting is configured to rotate with respect to the housing. A cable is in electrical communication with the camera head and is fixedly coupled to the pivot joint fitting and extends away from the camera head. A stand pole is fixedly coupled to the pivot joint fitting and extends away from the camera head.

Abstract: Pivot mechanisms for tracking cameras are disclosed herein. A tracking camera assembly includes a camera head having a housing and a pivot joint disposed within the housing. The pivot joint fitting is configured to rotate with respect to the housing. A cable is in electrical communication with the camera head and is fixedly coupled to the pivot joint fitting and extends away from the camera head. A stand pole is fixedly coupled to the pivot joint fitting and extends away from the camera head.

Abstract: A spacecraft architecture and accompanying standard allows for the creation of a spacecraft using an assortment of modules that comply with the standard. The standard preferably includes both mechanical and electrical compatibility criteria. To assure physical/mechanical compatibility, the structure of each module is constrained to be compatible with any other compatible module. To minimize the interference among modules, the extent of each module in select dimensions is also constrained. To assure functional compatibility, a common communication format is used to interface with each module, and each public-function module is configured to respond to requests for function capabilities that it can provide to other functions. Each module is preferably designed to provide structural support to the assemblage of modules, and an anchor module is provided or defined for supporting the entire assemblage and coupling the assemblage to other structures, such as a launch vehicle.