Spacecraft propulsion

Results: 2227



#Item
71Space Thruster Based on Inertial Electrostatic Confinement Benjamin A. Ulmen, Guilherme Amadio, Hugo Leon, George Chen, William W. Matisiak, Paul Keutelian, George H. Miley Introduction Theory of Operation

Space Thruster Based on Inertial Electrostatic Confinement Benjamin A. Ulmen, Guilherme Amadio, Hugo Leon, George Chen, William W. Matisiak, Paul Keutelian, George H. Miley Introduction Theory of Operation

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Source URL: fti.neep.wisc.edu

Language: English - Date: 2010-01-20 18:11:48
72プラズマ核融合学会誌3月【83-3】/目次

プラズマ核融合学会誌3月【83-3】/目次

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Source URL: www.jspf.or.jp

Language: English - Date: 2007-03-28 01:43:00
73Index active subspace analytic examples, 25 choosing the dimension, 6, 37, 59 computing, 25–35

Index active subspace analytic examples, 25 choosing the dimension, 6, 37, 59 computing, 25–35

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Source URL: www.siam.org

Language: English - Date: 2015-03-17 12:37:00
74Failure Knowledge DatabaseSelected Cases  Explosion of the Space Shuttle Challenger [January 28, 1986, USA] by Masayuki Nakao (Tokyo University, Institute of Engineering Innovation)

Failure Knowledge DatabaseSelected Cases Explosion of the Space Shuttle Challenger [January 28, 1986, USA] by Masayuki Nakao (Tokyo University, Institute of Engineering Innovation)

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Source URL: www.sozogaku.com

Language: English - Date: 2011-03-25 06:14:56
75Spacecraft / Anchor / Technology / Spaceflight / Satellites / Electrodynamic tether / Momentum exchange tether / Transport / Tether / Spacecraft propulsion

In-Store Update This activity uses attendees to learn about a specific child restraint and then share what they learned with the group. Depending on the number of attendees and CRs, this can be done individually or as a

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Source URL: cpsboard.org

Language: English - Date: 2015-04-09 17:12:34
76D3-GEO  GEO Platform, 35,786km Orbital Altitude, 15 Years Nominal Operational Life Dual-Pulse Re-Orbit Maneuver To 300 km Higher Graveyard Orbit

D3-GEO GEO Platform, 35,786km Orbital Altitude, 15 Years Nominal Operational Life Dual-Pulse Re-Orbit Maneuver To 300 km Higher Graveyard Orbit

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Source URL: www.deorbitaldevices.com

Language: English - Date: 2014-09-29 12:31:43
77BAYERN-CHEMIE GMBH MISSILE & SPACE PROPULSION SYSTEMS The performance of propulsion systems largely determines the capability of missiles and space transportation systems. Within MBDA, Bayern-Chemie is the competence cen

BAYERN-CHEMIE GMBH MISSILE & SPACE PROPULSION SYSTEMS The performance of propulsion systems largely determines the capability of missiles and space transportation systems. Within MBDA, Bayern-Chemie is the competence cen

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Source URL: www.bayern-chemie.com

Language: English - Date: 2014-08-13 10:09:13
78Naval S&T: Delivering Disruptive Technologies with Affordable Asymmetric Advantages RADM Matthew Klunder Chief of Naval Research

Naval S&T: Delivering Disruptive Technologies with Affordable Asymmetric Advantages RADM Matthew Klunder Chief of Naval Research

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Source URL: www.defenseinnovationmarketplace.mil

Language: English - Date: 2013-05-01 10:58:12
79Space Technology AOCS-Components Astround Feinwerktechnik Adlershof GmbH Albert-Einstein-Str.12

Space Technology AOCS-Components Astround Feinwerktechnik Adlershof GmbH Albert-Einstein-Str.12

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Source URL: www.astrofein.com

Language: English - Date: 2011-01-26 08:42:18
80ESA TECHNOLOGIES FOR SPACE DEBRIS REMEDIATION K. Wormnes(1) , R. Le Letty(1) , L. Summerer(1) , R. Schonenborg(1) , O. Dubois-Matra(1) , E. Luraschi(1) , A. Cropp(1) , H. Krag(2) , and J. DelavalESA/ESTEC, Keple

ESA TECHNOLOGIES FOR SPACE DEBRIS REMEDIATION K. Wormnes(1) , R. Le Letty(1) , L. Summerer(1) , R. Schonenborg(1) , O. Dubois-Matra(1) , E. Luraschi(1) , A. Cropp(1) , H. Krag(2) , and J. DelavalESA/ESTEC, Keple

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Source URL: www.esa.int

Language: English - Date: 2013-10-11 21:10:05