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Flight Motor Set 360l003 Sts 29r
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781724215413 Total Pages :328 pages Book Rating :4.2/5 (154 download)
Book Synopsis Flight Motor Set 360l003 (Sts-29r) by : National Aeronautics and Space Administration (NASA)
Download or read book Flight Motor Set 360l003 (Sts-29r) written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 328 pages. Available in PDF, EPUB and Kindle. Book excerpt: The redesigned solid rocket motor (RSRM) flight set 360L003 was launched on March 13, 1989 as part of NASA space shuttle mission STS-29R. As was the case with flight sets 360L001 and 360L002 (STS-26R and STS-27R), both motors (360L003A and 360L003B) performed in an excellent manner. Evaluation of the ground environment instrumentation measurements verified thermal model analysis data and showed agreement with predicted environmental effects. The right-hand aft field joint primary heater failed during the countdown; the secondary heater was activated and performed as designed. All other field joint heaters and aft skirt thermal conditioning systems had no anomalies. Shuttle thermal imager infrared readings compared favorably with measured ground environment instrumentation data. No thermal launch commit criteria violations occurred at any time. Evaluation of the development flight instrumentation showed exceptional propulsion performance. All ballistic parameters closely matched the predicted values and were well within the required specification levels. Girth and biaxial strain gage measurements compared closely with corresponding gages on previous flight motors, static tests, and with preflight predictions. Adequate safety factors were verified. (Some ignition transient spiking was noted in a few girth gages; the spiking was determined not to be representative of actual case behavior, but an instrumentation phenomena.) The accelerometers again measured high vibration amplitude levels during the ignition transient and the reentry Max Q phases. Postflight inspection showed that all combustion gas was contained by the insulation in the field and case-to-nozzle joints. No anomalous insulation erosion patterns were found, and the seals that did directly contain motor pressure showed no heat effects, erosion, or blowby. All anomalies identified were a result of splashdown damage, with the exception of fretting in the case field joint interference (nonsealing) surfaces an...
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1990 with total page 980 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1995 with total page 1100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1995 with total page 1096 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by : United States. Superintendent of Documents
Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1995 with total page 754 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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Download or read book Government Reports Annual Index written by and published by . This book was released on 1990 with total page 1120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis FY 1989 Scientific and Technical Reports, Articles, Papers, and Presentations by :
Download or read book FY 1989 Scientific and Technical Reports, Articles, Papers, and Presentations written by and published by . This book was released on 1989 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements & Index by :
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1990 with total page 1208 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flight Motor Set 360l009 (Sts-36). Volume 1 by : National Aeronautics and Space Adm Nasa
Download or read book Flight Motor Set 360l009 (Sts-36). Volume 1 written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-11-22 with total page 178 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight Motor Set 360L009, as part of NASA Space Shuttle Mission STS-36, a Department of Defence mission, was launched after two launch attempts. One launch was scrubbed following the failure of a ground-based Range Safety computer and one was scrubbed due to cloud cover at the return to launch landing site. As with all previous redesigned solid rocket motor launches, overall motor performance was excellent. There were no debris concerns from either motor. All ballistic and mass property parameters that could be assessed, closely matched the predicted values and were well within the required contract item specification levels. All field joint heaters and igniter joint heaters performed without anomalies. Evaluation of the ground environment instrumentation measurements again verified thermal model analysis data and showed agreement with predicted environmental effects. No launch commit criteria violations occurred. Postflight inspection again verified nominal performance of the insulation, phenolics, metal parts, and seals. Postflight evaluation indicated that both nozzles performed as expected during flight. All combustion gas was contained by insulation in the field and case-to-nozzle joints. Recommendations were made concerning improved thermal modeling and measurements. The rationale for these recommendations and complete result details are presented. Garecht, Diane M. POSTLAUNCH REPORTS; PROPULSION SYSTEM PERFORMANCE; SOLID PROPELLANT ROCKET ENGINES; SPACE SHUTTLE MISSIONS; SPACE TRANSPORTATION SYSTEM FLIGHTS; SPACECRAFT LAUNCHING; ENVIRONMENT EFFECTS; FAILURE; GENERAL OVERVIEWS; LANDING SITES; LAUNCHING SITES; POSTFLIGHT ANALYSIS; SPACECRAFT PERFORMANCE; THERMAL ANALYSIS...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723080074 Total Pages :176 pages Book Rating :4.0/5 (8 download)
Book Synopsis Flight Motor Set 360l009 (Sts-36). Volume 1 by : National Aeronautics and Space Administration (NASA)
Download or read book Flight Motor Set 360l009 (Sts-36). Volume 1 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight Motor Set 360L009, as part of NASA Space Shuttle Mission STS-36, a Department of Defence mission, was launched after two launch attempts. One launch was scrubbed following the failure of a ground-based Range Safety computer and one was scrubbed due to cloud cover at the return to launch landing site. As with all previous redesigned solid rocket motor launches, overall motor performance was excellent. There were no debris concerns from either motor. All ballistic and mass property parameters that could be assessed, closely matched the predicted values and were well within the required contract item specification levels. All field joint heaters and igniter joint heaters performed without anomalies. Evaluation of the ground environment instrumentation measurements again verified thermal model analysis data and showed agreement with predicted environmental effects. No launch commit criteria violations occurred. Postflight inspection again verified nominal performance of the insulation, phenolics, metal parts, and seals. Postflight evaluation indicated that both nozzles performed as expected during flight. All combustion gas was contained by insulation in the field and case-to-nozzle joints. Recommendations were made concerning improved thermal modeling and measurements. The rationale for these recommendations and complete result details are presented. Garecht, Diane M. Unspecified Center POSTLAUNCH REPORTS; PROPULSION SYSTEM PERFORMANCE; SOLID PROPELLANT ROCKET ENGINES; SPACE SHUTTLE MISSIONS; SPACE TRANSPORTATION SYSTEM FLIGHTS; SPACECRAFT LAUNCHING; ENVIRONMENT EFFECTS; FAILURE; GENERAL OVERVIEWS; LANDING SITES; LAUNCHING SITES; POSTFLIGHT ANALYSIS; SPACECRAFT PERFORMANCE; THERMAL ANALYSIS...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723079153 Total Pages :166 pages Book Rating :4.0/5 (791 download)
Book Synopsis Flight Motor Set 360l007 (Sts-33r) by : National Aeronautics and Space Administration (NASA)
Download or read book Flight Motor Set 360l007 (Sts-33r) written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight motor set 360L007 was launched as part of NASA space shuttle mission STS-33R. As with all previous redesigned solid rocket motor launches, overall motor performance was excellent. There were no debris concerns for either motor. Both motors exhibited unbonds on one factory joint weatherseal. All ballistics contract end item specification parameters were verified, with the exception of ignition interval and rise rates. Ignition interval and rise rates could not be verified due to the elimination of developmental flight instrumentation from fourth flight and subsequent, but the low sample rate data that were available showed nominal propulsion performance. All ballistic and mass property parameters closely matched the predicted values and were well within the required contract end item specification levels that could be assessed. All 108 Ground Environment Instrumentation (GEI) measurements performed properly throughout the prelaunch phase. Evaluation of the GEI measurements again verified thermal model analysis data and showed agreement with predicted environmental effects. No launch commit criteria thermal violations occurred. All joint heaters operated normally, but a high voltage reading was noted on the left hand aft heater, which was immediately determined to be a voltage sensor error and not a heater anomaly due to no current increase. Postflight inspection again verified superior performance of the insulation, phenolics, metal parts, and seals. Postflight evaluation indicated both nozzles performed as expected during flight. All combustion gas was contained by insulation in the field and case-to-nozzle joints. Garecht, Diane Unspecified Center BALLISTICS; COMBUSTION; FLIGHT INSTRUMENTS; IGNITION; INSULATION; LAUNCHING; SOLID PROPELLANT ROCKET ENGINES; SPACE SHUTTLES; SPACE TRANSPORTATION SYSTEM FLIGHTS; THERMAL ANALYSIS; ANOMALIES; DEBRIS; ELECTRIC POTENTIAL; ENVIRONMENT EFFECTS; ERRORS; HEATERS; HIGH VOLTAGES; INSPECTION; PROPULSION; SPECIFICATIONS...
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781724214881 Total Pages :372 pages Book Rating :4.2/5 (148 download)
Book Synopsis Flight Motor Set 360l001 (Sts-26r). Volume 5 by : National Aeronautics and Space Administration (NASA)
Download or read book Flight Motor Set 360l001 (Sts-26r). Volume 5 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-24 with total page 372 pages. Available in PDF, EPUB and Kindle. Book excerpt: A review of the performance and post-flight condition of the STS-26 Redesigned Solid Rocket Motor (RSRM) nozzles is presented. The nozzle assemblies, flown on the Space Shuttle Discovery on 29 September 1988, were tested to demonstrate flex bearing system reusability. The evaluation indicated no condition that would adversely affect the reusability of the flex bearing system. Inspection showed that the flex bearings did not leak, were not damaged by water impact, had the expected erosion profiles, and that the remaining ablative liner thicknesses met the performance margin of safety. Applicable Discrepancy Reports and Process Departures, the Nozzle Component Program Team performance evaluation, and the Redesign Program Review Board assessment are included. George, Russell J. Unspecified Center NASA-CR-183771, NAS 1.26:183771, TWR-17272-VOL-5 NAS8-30490...
