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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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This viewgraph reviews the current missions that JPL is managing for NASA. Specifically it reviews JPL's capabilities end-to-end to implement missions, development of research and technology. It includes information on JPL's vision for space exploration and JPL's current missions It reviews the recent scientific findings. Lastly, the presentation gives an overview of the Mars Science Laboratory Mission.
For a number of years ongoing bibliographies of various JPL missions (AIRS, ASTER, Cassini, GRACE, Earth Science, Mars Exploration Rovers (Spirit & Opportunity)) have been compiled by the JPL Library. Mission specific bibliographies are compiled by the Library and sent to mission scientists and managers in the form of regular (usually quarterly) updates. Charts showing publications by years are periodically provided to the ASTER, Cassini, and GRACE missions for supporting Senior Review/ongoing funding requests, and upon other occasions as a measure of the impact of the missions. Basically the Web of Science, Compendex, sometimes Inspec, GeoRef and Aerospace databases are searched for the mission name in the title, abstract, and assigned keywords. All get coded for journal publications that are refereed publications.
MONTE (Mission analysis, Operations, and Navigation Toolkit Environment) is a new software system being developed to replace the navigation and trajectory analysis software currently in use at the Jet Propulsion Laboratory (JPL). MONTE will reproduce the existing functionality of the legacy systems and add significant new capabilities for the MONTE users - the mission and navigation analysts in the Navigation and Mission Design Section (Section 312). MONTE will be developed as a single tightly integrated system, in contrast to the multiple disparate software suites currently in use. MONTE is being designed to facilitate a variety of navigation and trajectory tasks in a broad range of contexts, including research and development, analysis and design, and operations.
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Since the success of the DS1 mission, electric propulsion (EP) has moved from the laboratory to application on many present and proposed JPL missions.
This paper discusses the following topics: (1) Autonomy for Future Missions- Mars Outposts, Titan Aerobot, and Europa Cryobot / Hydrobot; (2) Emergence of Autonomy- Remote Agent Architecture, Closing Loops Onboard, and New Millennium Flight Experiment; and (3) Software Engineering Challenges- Influence of Remote Agent, Scalable Autonomy, Autonomy Software Validation, Analytic Verification Technology, and Autonomy and Software Software Engineering.
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The overall objective of the proposed effort is to develop a flexible microactuator based on tailored films of lead lanthanum zirconate titanate, PLZT (deposited on flexible substrates) and to demonstrate a multifold enhancement in its force/discplacement capabilities, compared to those of the current state-of-the-art actuators based on bulk ceramic materials.
Future space programs place a variety of needs on storage technologies.
Over the last several decades, engineers at the Jet Propulsion Laboratory have developed a collection of analytical tools to design missions to Earth orbit, the moon, sun, planets and various other bodies in our solar system, and beyond.
The Mars Climate Orbiter (MCO) was launched on December 11, 1998. The MCO was to arrive at Mars and begin orbit insertion on September 23, 1999. The Mars Orbit Insertion (MOI) burn, a 16-minute maneuver to slow the spacecraft and enable capture into an orbit around Mars, began on schedule. Five minutes into the maneuver, and approximately 49 seconds before the anticipated time for loss of communication, the MCO was occulted by Mars. Thereafter, no contact with the spacecraft could be established. On September 24, 1999, an internal JPL team (the MCO Peer Review Team) was appointed to help investigate the reason for the loss of spacecraft signal. The Peer Review Team's findings are presented in this report.
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Mission Design and Navigation at the Jet Propulsion Laboratory has implemented an automation framework tool to assist in orbit determination and maneuver design analysis. This paper describes the lessons learned from previous automation tools and how they have been implemented in this tool. In addition this tool has revealed challenges in software implementation, testing, and user education. This paper describes some of these challenges and invites others to share their experiences.
Today there are may small deep space missions in progress or in conception at the Jet Propulsion Laboratory.