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Stocky, J. F.

Publications and source records attributed to Stocky, J. F..

Technology readiness levels for the new millennium program

NASA's New Millennium Program (NMP) seeks to advance space exploration by providing an in-space validating mechanism to verify the maturity of promising advanced technologies that cannot be adequately validated with Earth-based testing alone. In meeting this objective, NMP uses NASA Technology Readiness Levels (TRL) as key indicators of technology advancement and assesses development progress against this generalized metric. By providing an opportunity for in-space validation, NMP can mature a suitable advanced technology from TRL 4 (component and/or breadboard validation in laboratory environment) to a TRL 7 (system prototype demonstrated in an Earth-based space environment). Spaceflight technology comprises a myriad of categories, types, and functions, and as each individual technology emerges, a consistent interpretation of its specific state of technological advancement relative to other technologies is problematic.

technology readiness TRL New Millennium Program NM

An overview of NASA's activities in micro-nano technologies

An examination of how mass is used in spacecraft design indicates that technology efforts directed only to reduce the mass of electronics, both digital and analog will not significantly reduce the mass of a spacecraft, regardless of how much success those efforts achieve.

micro-nano technology

NASA's Telerobotic Testbed

As part of the Advanced Technology Program in Telerobotics Technology conducted by NASA's Office of Aeronautics and Space Technology, a Telerobotics Testbed has been placed into use at the Jet Propulsion Laboratory. The Telerobotics Testbed represents an integration of the discipline technologies represented by its subsystems: (1) Operator Control Station, (2) Planning and Reasoning, (3) Run Time Control, (4) Sensing and Perception, and (5) Manipulation and Control Mechanization. The features provided initially by the Telerobotic Testbed are described both at the subsystem level and at the level of a fully integrated, end-to-end system. The capabilities of the total system as displayed experimentally are discussed, and the capabilities of which the Telerobotic Testbed will be capable are described. The experimental program to define the performance of the Telerobotic Testbed is discussed.

Stocky, J. F.

Highlights of NASA research in telerobotics

This paper provides a brief overview of the NASA program of research in telerobotics. It describes ongoing effort in a number of participating laboratories investigating topics in human-machine interaction, intelligent task planning and execution, dual-arm control of manipulators with redundant degrees-of-freedom, sensing and perception. A brief list of illustrative references is provided.

Weisbin, C. R.

Future spacecraft propulsion

Propulsion requirements for launch vehicles, upper stages, satellites and platforms, and planetary spacecraft are described from a functional perspective and compared on an energy basis. Mission velocity requirements for a range of missions are presented. A simple model relating optimum exhaust velocity and maximum system delta-V as a function of system-specific energy is developed, which provides insight into the relationship between system performance and various power and propulsion subsystem characteristics. Based on this model, various advanced propulsion options, e.g., the solid-core nuclear rocket and nuclear electric propulsion, are evaluated, and the implications of this analysis for propulsion and power system technology development programs are discussed. The objective of this paper is to provide an overview of future propulsion requirements for the nonspecialist.

Garrison, P. W.