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AIAA Journal, ISSN 0001-1452, 04/1990, Volume 28, Issue 4, pp. 717 - 724
Journal Article
Journal of Geophysical Research: Oceans, ISSN 0148-0227, 12/1994, Volume 99, Issue C12, pp. 24895 - 24906
The NASA altimeter on board TOPEX/POSEIDON exploits the difference in the delays of the Ku and C band radar pulses to estimate an ionosphere correction to the... 
SPACECRAFT DESIGN, TESTING AND PERFORMANCE | OCEANOGRAPHY
Journal Article
Journal of Guidance, Control, and Dynamics, ISSN 0731-5090, 09/1985, Volume 8, Issue 5, pp. 620 - 627
A method called the eigensystem realization algorithm is developed for modal parameter identification and model reduction of dynamic systems from test data. A... 
SPACECRAFT DESIGN, TESTING AND PERFORMANCE | Parameter identification | Algorithms | Model reduction
Journal Article
AIAA Journal, ISSN 0001-1452, 10/1987, Volume 25, Issue 10, pp. 1373 - 1385
Journal Article
07/2015
The Amine Swingbed Payload is an experimental system deployed on the International Space Station (ISS) that includes a two-bed, vacuum regenerated, amine-based... 
Spacecraft Design, Testing and Performance
Conference Proceeding
03/2014
NASA's Morpheus Project has developed and tested a prototype planetary lander capable of vertical takeoff and landing, that is designed to serve as a testbed... 
Spacecraft Design, Testing and Performance
Conference Proceeding
08/2014
The Autonomous precision Landing and Hazard Avoidance Technology (ALHAT) project has developed a suite of prototype sensors for enabling autonomous and safe... 
Spacecraft Design, Testing and Performance
Conference Proceeding
Journal of Guidance, Control, and Dynamics, ISSN 0731-5090, 09/1993, Volume 16, Issue 5, pp. 852 - 858
A new method is described for assessing the consistency of structural modal parameters identified with the eigensystem realization algorithm. Identification... 
SPACECRAFT DESIGN, TESTING AND PERFORMANCE | IDENTIFICATION | AEROSPACE ENGINEERING & TECHNOLOGY | INSTRUMENTS & INSTRUMENTATION | Algorithms
Journal Article
01/2014
One of NASA Johnson Space Center's test articles of the amine-based carbon dioxide (CO2) and water vapor sorbent system known as the CO2 And Moisture Removal... 
Spacecraft Design, Testing and Performance
Conference Proceeding
07/2014
NASA's Edison program is intending to launch the Edison Demonstration of Smallsat Networks (EDSN) project, a swarm of 8 1.5U cubesats in the fall of 2014 to... 
Spacecraft Design, Testing and Performance
Conference Proceeding
01/2015
The Orion Multi-Purpose Crew Vehicle is susceptible to ipping apex forward between drogue parachute release and main parachute in ation. A smart drogue release... 
Spacecraft Design, Testing and Performance
Conference Proceeding
01/2014
The CubeSat form factor of nanosatellite (a satellite with a mass between one and ten kilograms) has grown in popularity due to their ease of construction and... 
Spacecraft Design, Testing and Performance
Conference Proceeding
AIAA Journal, ISSN 0001-1452, 05/1994, Volume 32, Issue 5, pp. 1049 - 1057
A method is presented by which measured modes and frequencies from a modal test can be used to determine the location and magnitude of damage in a space struss... 
SPACECRAFT DESIGN, TESTING AND PERFORMANCE | EIGENSTRUCTURE ASSIGNMENT | STIFFNESS | IDENTIFICATION | ADJUSTMENT | AEROSPACE ENGINEERING & TECHNOLOGY | FINITE-ELEMENT MODELS | Eigenvectors | Research | Strains and stresses | Analysis | Trusses
Journal Article
01/2014
Spacecraft multibody separation events during atmospheric descent require complex testing and analysis to validate the flight separation dynamics model and to... 
Spacecraft Design, Testing and Performance
Conference Proceeding
08/2014
A consortium of innovative experts in additive manufacturing (AM) comprising Northrup Grumman Technical Services, University of Texas at El Paso (UTEP),... 
Spacecraft Design, Testing and Performance
Conference Proceeding
01/2015
A woven Vectran inflatable module 88 inches in diameter and 10 feet long was tested at the NASA Johnson Space Center until failure from creep. The module was... 
Spacecraft Design, Testing and Performance | Nonmetallic Materials
Conference Proceeding
08/2014
The Asteroid Robotic Redirect Mission (ARRM) has been the topic of many mission design studies since 2011. The reference ARRM spacecraft uses a powerful solar... 
Spacecraft Design, Testing and Performance
Conference Proceeding
08/2014
Variances in atmospheric density are directly related to the variances in solar flux intensity between 11- year solar cycles. The Orbital Debris Engineering... 
Spacecraft Design, Testing and Performance
Conference Proceeding
06/2014
Todays presentation describes preliminary results from a study of extreme auroral charging in low Earth orbit. Goal of study is to document characteristics of... 
Spacecraft Design, Testing and Performance
Conference Proceeding
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