Asteroid Redirect Mission - NASA
• Demonstrate)high8power)Solar)Electric) Propulsion)(SEP).) • Demonstrate)the)ability)to)capture)large) non8cooperative)objectsin)deep)space objective) of) looking) at the) asteroid) redirect mission) concept in) sufficient depth) to) determine)if)its)feasibility)would)stand)up)to ... Access Document
Small Satellite Design For Inner Solar System Exploration
SMALL SATELLITE DESIGN FOR INNER SOLAR SYSTEM EXPLORATION SOLAR ELECTRIC PROPULSION 268.3 kg 29.8 kg 73.8 kg Initial Solar Electric Propulsion Design Masses Xenon-ion engine module 10 kW EOL solar array Earth escape fuel ... Read Full Source
Statement Of R. Joseph Cassady
Solar Electric Propulsion (SEP) is key to a sustainable architecture by enabling efficient transfer of cargo, habitats and payloads to The NEXT-C xenon ion engine system is tailored to the needs of NASA’s Science Mission Directorate. ... Doc Retrieval
The Dawn Ion Propulsion System - Springer
The system includes three 30-cm diameter xenon ion thrusters and two Power Processor Units (PPUs) of the type developed by the NASA Solar electric propulsion Tech-nology Application Readiness (NSTAR) Project (Brophy et al. 2000) and flight-tested on ... Return Document
Characterization Of The NASA NEXT Thruster
NSTAR = NASA Solar Electric Propulsion Technology Application Readiness Program P in-PPU XIPS = Xenon Ion Propulsion System η = efficiency *Senior Scientist, 5 Joint Propulsion ... Read Content
Ion Thruster - Wikipedia
An ion thruster or ion drive is a form of electric propulsion used for spacecraft propulsion. Nuclear Electric Xenon Ion System (NEXIS) High Power Electric Propulsion Based on the NASA design criteria, Hughes Research Labs, developed the Xenon Ion Propulsion System (XIPS) ... Read Article
Panvig The Way For FUTURE EXPLORATION
Objective of SMART-1 was to demonstrate the use of solar-electric propulsion on a deep space trajectory, taking the spacecraft from the Earth to the Moon, using a single Xenon ion thruster, SMART-1 travelled 82 million km in its spiral trajectory to the Moon. Image courtesy ESA. ... View This Document
NASA’s Deep Space 1 Ion Engine (plenary)
NASA’s Deep Space 1 ion engine —plenary The first use of solar electric propulsion ~SEP! on a The DS1 spacecraft uses a single xenon ion engine, provided by the NASA Solar Elec-tric Propulsion Technology Applications Readiness ~NSTAR! ... Retrieve Here
AdvancedPropulsion For GeostationaryOrbitInsertion AndNorth ...
Solar electric propulsion technology is currently being used for geostationmT satellite station keeping. system, or a xenon ion system, which also performs 15 years of sta-tion keeping. The analyses used conservative assumptions for these ... Read Here
AIM-2003-455 8 - JPL TRS Home
AIM-2003-455 8 STATUS OF THE EXTENDED LIFE TEST OF THE DEEP SPACE 1 FLIGHT flying a 30-cm-diameter Xenon Ion Engine as its primary propulsion system. utilizing solar electric propulsion to demand lifetimes and ... Fetch Doc
Appendix A Nomenclature - NASA
Appendix A Nomenclature A.1 Constants A v Avogadro’s number (atoms/mole) NEXIS Nuclear Electric Xenon Ion Thruster System NEXT NASA’s Evolutionary Xenon Thruster NSTAR NASA Solar Electric Propulsion Technology Applications Readiness PG pyrolytic graphite PIC particle in cell ... Document Viewer
Dawn's Xenon Ion Thrusters - YouTube
Celestia particle system demonstration: ion thrusters on the Dawn spacecraft. Solar electric propulsion is the enabling technology for Dawn's mission to the ... View Video
Air Breathing Ion Engine Concept - ZARM: ZARM
Air Breathing Ion Engine Concept Kazutaka Nishiyama nishiyama@ep.isas.ac.jp A completely new solar electric propulsion (SEP) concept, the Air Breathing Ion Engine (ABIE), has been proposed for spacecraft drag makeup. compared to conventional xenon ion propulsion systems. ... Access Doc
Charge Exchange Ions Produced By An Ion Propulsion System
These include the first use of solar electric ion propulsion system for primary propulsion, and a low-resource plasma spectrometer and time of The 30-cm diameter, xenon ion propulsion system on Deep Space One by the NSTAR program, a collaboration between NASA ... Fetch Doc
Performance Evaluation Of An Expanded Range XIPS Ion Thruster ...
This paper examines the benefit that a solar electric propulsion (SEP) system based on the 5 kW Xenon Ion Propulsion System (XIPS) could have for NASA’s Discovery class deep space missions. The relative cost and performance of the commercial heritage XIPS system ... Fetch Document
Preliminary Design Of Nuclear Electric Propulsion Missions To ...
Preliminary Design of Nuclear Electric Propulsion Missions by Kawaguchi,18 Sauer,19 Williams and Coverstone-Carroll,20 and Maddock and Sims.21 In solar electric propulsion Electric Xenon Ion System3 (NEXIS). See Table 1. We assume ... Doc Viewer
Planetary Mission Performance For Small Solar Electric ...
Planetary Mission Performance for Small Solar Electric Propulsion Spacecraft Carl G. Sauer, Jr Jet Propulsion Laboratory California Institute of Technology propulsion thruster technology together with a proposed flight test of a Xenon ion thruster on an Air Force mission (SSTAR) ... Content Retrieval
Deep Space 1 - Atk.com
Camera, an imaging spectrometer, and the Xenon Ion Propulsion System (XIPS). The XIPS provided about 10 times the specific impulse (ratio of thrust to propellant used) of that of chemical propulsion. • Solar Electric (xenon ion) Propulsion. ... Read Full Source
Universe - Jet Propulsion Laboratory
The award went to the Solar Electric Propulsion Technology Application Readiness (NSTAR) program team, which developed and delivered Deep Space 1’ s ion propul- develop xenon ion engines for deep-space missions. In June 1996, a prototype engine built by ... Fetch This Document
Chapter 1 Introduction - DESCANSO
Chapter 1 Introduction Electric propulsion is a technology aimed at achieving thrust with high exhaust Xenon Ion Propulsion System (XIPS) [17], and the first NASA deep-space mission using the NASA Solar Electric Propulsion Technology Applications Readiness (NSTAR) ... Fetch Doc
Integrated Vehicle And Trajectory Design Of Small Spacecraft ...
Craft using emerging small solar electric propulsion technologies. Xenon Ion (MiXI) [7], Integrated Vehicle and Trajectory Design of Small Spacecraft with Electric Propulsion for Earth and Interplanetary Missions ... Access Full Source
NEXT Ion Propulsion System Development Status - NASA
This paper describes the NEXT ion propulsion system development status, NSTAR = NASA Solar Electric Propulsion Technology Application Readiness diameter, xenon ion thruster with 2-grid ion optics. The beam ... Fetch Content
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