Vibration test of a breadboard gimbal for the NEXT ion engine

Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference

Volumn 5, Issue , 2006, Pages 3424-3432

  Snyder, John Steven ^a,c,d   O'Connell, Michael R ^a,e   Fernandez, Juan P ^a,e   Wang, Gary ^b   McNabb Jr , Richard S ^b,d,f   Crumb, Dustin ^b,g  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^b Swales Aerospace   (United States)

^c Advanced Propulsion Technology Group   (United States)

^d AIAA   (United States)

^e Dynamics Environments Group   (United States)

^f Mechanical Systems

^g Mechanical Systems Engineer   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; ION PROPULSION; MATHEMATICAL MODELS; ROBOTICS; SOLAR SYSTEM; VIBRATIONAL SPECTRA;

ION ENGINE; ROBOTIC EXPLORATION; SOLAR ELECTRIC POWER;

AIRCRAFT ENGINES;

EID: 34249009223     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-4665     Document Type: Conference Paper

References (4)

1. st Joint Propulsion Conference, Tucson, AZ, July 2005.
2. th Joint Propulsion Conference, Fort Lauderdale, FL, July 2004.
3. st Joint Propulsion Conference, Tucson, AZ, July 2005.
4. NASA-HDBK-7004B, "Force Limited Vibration Testing," NASA Technical Handbook, January 31, 2003.