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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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Deep Space 1 photometry of Comet Borrelly: taking Hapke modeling to the limit
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Deep Space 1 telecom link analysis: enabler of spacecraft mission recovery and ground station performance maintenance
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A review of the Deep Space 1 mission: important results in spacecraft engineering and space science
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Flight Software Implementation of the Beacon Operations Experiment on the NASA New Millennium Deep Space 1 (DS-1) Mission
This paper will describe the implementation approach of the beacon monitor experiment on the DS-1 spacecraft.
Orbit Determination Performance Evaluation of the Deep Space 1 Autonomous Navigation System
NASA's New Millennium Program involves a series of missions whose primary purpose is to demonstrate the feasibility of new technologies for spaceflight.
The Deep Space 1 Autonomous Navigation System: A Post-Flight Analysis
NASA's New Millenium Program consists of a series of missions whose primary purpose is to demonstrate the feasibility of new technologies for space flight.
Performance characteristics of the deep space 1 flight spare ion thruster long duration test, the first 21,300 hours of operation
A long duration test of the DSl flight spare ion thruster (FT2) is presently being conducted at the Jet Propulsion Laboratory. To, date the thruster has accumulated over 23,500 hours of operation, and 190 kg of Xenon propellant, over 230% of the initial design life. The primary objectives of the test include the processing of 200 kg of Xenon propellant, the identification of unknown failure modes, the characterization and drivers of these failure modes, and to measure performance degradation as the thruster wears. The test is fitted with an extensive array of diagnostics to measure engine wear and performance degradation. To date the most notable erosion processes include severe discharge cathode keeper erosion, accelerator grid erosion, reduction in electrical isolation of the neutralizer assembly, and deposit formation within the neutralizer orifice, reducing margin from plume mode. Over the past 23,500 hours of operation, performance degradation has been minimal, and it is anticipated that the above erosion processes will not preclude the thruster from processing over 200 kg of Xenon.
Deep Space 1 Mission and observation of Comet Borrelly
After DS1 1 completed its successful primary mission in 1999, NASA sent it on a risky and ambitious extended mission to conduct comet science. In September 2001, DSl executed a flawless encounter with comet Borrelly, yielding the best pictures and other scientific data ever collected at a comet, providing scientists with a tremendous advance in our understanding of these intriguing and important parts of the solar system.
Deep Space 1 flight experience: adventures on an ion drive (AAS 02-072)
This paper provides a brief overview of the DSI attitude control subsystem, shares a few lessons-learned, and describes some of the many daunting challenges faced by our tiny flight team during the course of the mission. Special focus will be given to the nuances of flying a spacecraft with ion propulsion, our nick-of-time rewrite of the attitude determination software after the failure of the on-board star tracker in late 1999, and DSl's subsequent successful flyby of comet Borrelly on September 22, 2001.
Deep Space 1 flight experience: adventures on an ion drive (AAS 02-072) - viewgraphs
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Navigation of the Deep Space 1 spacecraft at Borrelly
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NASA's Deep Space 1 ion engine
Derivatives of the NSTAR ion engine are being evaluated to assess their capability to meet future needs.
Deep Space 1 Mission Overview
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Deep Space 1 Mission Overview
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Ion Propulsion Subsystem Environmental Effects on Deep Space 1: Initial Results from the IPS Diagnostics Subsystem
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Deep Space 1 Autonomous Navigation
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