Search Results

Matching Records: 252
1 2 3 4 5 6 7 8 9 10 Next >>
Sort Results By:
Selected   › View Selected  /  › Clear Selected
Sub-scale Waterflow Cavitation and Dynamic Transfer Function Testing of an Oxidizer Turbo-Pump Combined Inducer and Impeller
Document ID: 20170000426
NTRS Full-Text: Click to View  [PDF Size: 7 KB]
Author: Karon, D. M.; Patel, S. K.; Zoladz, T. F.
Abstract: In 2009 and 2010, Concepts NREC prepared for and performed a series of tests on a 52% scale of a hide
Publication Year: 2016
Document Type: Conference Paper
Report/Patent Number: M16-5435
Date Acquired: Jan 18, 2017
CFD Simulations of the Supersonic Inflatable Aerodynamic Decelerator (SIAD) Ballistic Range Tests
Document ID: 20170000395
NTRS Full-Text: Click to View  [PDF Size: 6.6 MB]
Author: Brock, Joseph; Stern, Eric; Wilder, Michael
Abstract: A series of ballistic range tests were performed on a scaled model of the Supersonic Flight hide
Publication Year: 2017
Document Type: Oral/Visual Presentation
Report/Patent Number: ARC-E-DAA-TN38596
Date Acquired: Jan 17, 2017
Experimental Comparison of Piezoelectric and Magnetostrictive Shunt Dampers
Document ID: 20170000337
NTRS Full-Text: Click to View  [PDF Size: 5.1 MB]
Author: Asnani, Vivake M.; Deng, Zhangxian; Scheidler, Justin J.; Dapino, Marcelo J.
Abstract: A novel mechanism called the vibration ring is being developed to enable energy conversion elements hide
Publication Year: 2016
Document Type: Conference Paper
Report/Patent Number: GRC-E-DAA-TN30479
Date Acquired: Jan 12, 2017
Experimental Comparison of Piezoelectric and Magnetostrictive Shunt Dampers
Document ID: 20170000021
NTRS Full-Text: Click to View  [PDF Size: 1.5 MB]
Author: Asnani, Vivake M.; Deng, Zhangxian; Dapino, Marcelo J.; Scheidler, Justin J.
Abstract: A novel mechanism called the vibration ring is being developed to enable energy conversion elements hide
Publication Year: 2016
Document Type: Oral/Visual Presentation
Report/Patent Number: GRC-E-DAA-TN30750
Date Acquired: Jan 04, 2017
Low Density Supersonic Decelerator (LDSD) Supersonic Flight Dynamics Test (SFDT) Plume Induced Environments Modelling
Document ID: 20160008865
NTRS Full-Text: Click to View  [PDF Size: 3.2 MB]
Author: Mobley, Brandon; Smith, Sheldon; Van Norman, John; Muppidi, Suman; Clark, Ian
Abstract: No abstract available
Publication Year: 2016
Document Type: Oral/Visual Presentation
Report/Patent Number: M16-5362
Date Acquired: Dec 19, 2016
Non-Invasive Tension Measurement Devices for Parachute Cordage
Document ID: 20160012716
NTRS Full-Text: Click to View  [PDF Size: 190 KB]
Author: Litteken, Douglas A.; Daum, Jared S.
Abstract: The need for lightweight and non-intrusive tension measurements has arisen alongside the development hide
Publication Year: 2016
Document Type: Conference Paper
Report/Patent Number: JSC-CN-37810
Date Acquired: Nov 01, 2016
Low Density Supersonic Decelerator (LDSD) Supersonic Flight Dynamics Test (SFDT) Plume Induced Environment Modelling
Document ID: 20160008864
NTRS Full-Text: Click to View  [PDF Size: 1.6 MB]
Author: Mobley, B. L.; Smith, S. D.; Van Norman, J. W.; Muppidi, S.; Clark, I
Abstract: Provide plume induced heating (radiation & convection) predictions in support of the LDSD hide
Publication Year: 2016
Document Type: Oral/Visual Presentation
Report/Patent Number: M16-5363
Date Acquired: Jul 12, 2016
Single-Event Effect Performance of a Conductive-Bridge Memory EEPROM
Document ID: 20160005843
NTRS Full-Text: Click to View  [PDF Size: 689 KB]
External Online Source:

Author: Chen, Dakai; Wilcox, Edward; Berg, Melanie; Kim, Hak; Phan, Anthony; Figueiredo, Marco; Seidleck, Christina; LaBel, Kenneth
Abstract: We investigated the heavy ion single-event effect (SEE) susceptibility of the industry’s first hide
Publication Year: 2015
Document Type: Accepted Manuscript
Report/Patent Number: GSFC-E-DAA-TN31700
Date Acquired: May 09, 2016
Lessons Learned Briefing PLSS 2.0
Document ID: 20160001782
NTRS Full-Text: Click to View  [PDF Size: 1022 KB]
Author: McMann, Joe
Abstract: No abstract available
Publication Year: 2012
Document Type: Oral/Visual Presentation
Report/Patent Number: JSC-CN-29360
Date Acquired: Feb 12, 2016
Impact Behavior of Composite Fan Blade Leading Edge Subcomponent with Thermoplastic Polyurethane Interleave
Document ID: 20150022907
NTRS Full-Text: Click to View  [PDF Size: 1.3 MB]
Author: Miller, Sandi G.; Roberts, Gary D.; Kohlman, Lee W.; Heimann, Paula J.; Pereira, J. Michael; Ruggeri, Charles R.; Martin, Richard E.; McCorkle, Linda S.
Abstract: Impact damage tolerance and damage resistance is a critical metric for application of polymer matrix hide
Publication Year: 2015
Document Type: Conference Paper
Report/Patent Number: GRC-E-DAA-TN22397
Date Acquired: Dec 14, 2015
1 2 3 4 5 6 7 8 9 10 Next >>
Facebook icon, External Link to NASA STI page on Facebook Twitter icon, External Link to NASA STI on Twitter YouTube icon, External Link to NASA STI Channel on YouTube RSS icon, External Link to New NASA STI RSS Feed
Refine By
Search History
 
NASA Logo, External Link

NASA Official: Gerald Steeman

Sponsored By: NASA Scientific and Technical Information Program

Site Curator: STI Support Services

Last Modified: March 28, 2017

Privacy Policy & Important Notices Disclaimers, Copyright, Terms of Use Freedom of Information Act USA.gov NASA.gov NASA OCIO Free Adobe PDF Reader Free MS Word Viewer