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Author : Anonim
Publisher : Unknown
Page : 660 pages
File Size : 51,8 Mb
Release : 1989
Category : Electronic
ISBN : NWU:35556030151526
Author : United States. General Accounting Office
Publisher : Unknown
Page : 24 pages
File Size : 40,5 Mb
Release : 1992
Category : Space shuttles
ISBN : UIUC:30112033980100
Author : National Aeronautics and Space Adm Nasa
Publisher : Unknown
Page : 106 pages
File Size : 41,6 Mb
Release : 2018-11-08
Category : Electronic
ISBN : 1731031874
The Space Shuttle Redesigned Solid Rocket Motor (RSRM) Certification Program provides confidence that the RSRM and its components/subsystems meet or exceed Mission Oriented Requirements when manufactured per design requirements and specified/approved processes. Certification is based on documented results of tests, analyses, inspections, similarity, and demonstrations. Evidencing information is provided to certify that each RSRM component/subsystem satisfies design, mission related requirements and objectives. Duersch, Fred, Jr. Unspecified Center CERTIFICATION; QUALIFICATIONS; ROCKET ENGINE DESIGN; SPACE SHUTTLE BOOSTERS; ENGINE PARTS; ENGINE TESTS; INSPECTION; MISSION PLANNING...
Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
Page : 54 pages
File Size : 52,5 Mb
Release : 2018-10-26
Category : Electronic
ISBN : 1729302092
This interim final report summarizes the activities and major accomplishments under NASA/MSFC Contract NAS8-39235 for the initial two year contractual effort beginning October 1, 1991, and ending September 30, 1993. It is not intended as an exhaustive treatment or review of any particular technical issue which was addressed during this two-year period, but does provide an overview of the many induced environment studies and test support activities undertaken by REMTECH and its subcontractors during this two-year period. The initial scope of work has been pursued vigorously through this two-year period by separating the effort into five functional areas. The five functional areas are ascent plume radiation, ascent plume convection, ascent aerodynamic heating, launch stand environments, and reentry heating. A work breakdown structure (WBS) for each functional area was devised to permit nearly autonomous activities within each functional responsibility while maintaining commonality in reporting procedures and cost accounting. The contract was modified 11 times to provide incremental funding and to expand the scope of work. Additional work breakdown structure was incorporated to meet the expanded scope. A contract chronology is provided in Section 2. The initial scope of work, expanded scope, and corresponding WBS designation are described in Section 3. A summary review of major accomplishments is also provided in Section 4 to show the breadth of activities and extent of reporting. Reports, meetings, test activities, and other accomplishments within each functional area are also summarized by WBS heading in the appendices. Unspecified Center
Author : United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Space Science and Applications
Publisher : Unknown
Page : 64 pages
File Size : 52,8 Mb
Release : 1988
Category : Astronautics
ISBN : PSU:000013397500
Author : United States. Congress. House. Committee on Government Operations. Legislation and National Security Subcommittee
Publisher : Unknown
Page : 356 pages
File Size : 43,9 Mb
Release : 1986
Category : Space shuttles
ISBN : PSU:000011993698
Author : United States. Congress. House. Committee on Science and Astronautics
Publisher : Unknown
Page : 80 pages
File Size : 50,7 Mb
Release : 1962
Category : Rockets
ISBN : LOC:00186796500
Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
Page : 126 pages
File Size : 49,7 Mb
Release : 2018-11-14
Category : Science
ISBN : 1731316135
Space Shuttle Flight Support Motor No. 1 (FSM-1) was static test fired on 15 Aug. 1990 at the Thiokol Corporation Static Test Bay T-24. FSM-1 was a full-scale, full-duration static test fire of a redesigned solid rocket motor. FSM-1 was the first of seven flight support motors which will be static test fired. The Flight Support Motor program validates components, materials, and manufacturing processes. In addition, FSM-1 was the full-scale motor for qualification of Western Electrochemical Corporation ammonium perchlorate. This motor was subjected to all controls and documentation requirements CTP-0171, Revision A. Inspection and instrumentation data indicate that the FSM-1 static test firing was successful. The ambient temperature during the test was 87 F and the propellant mean bulk temperature was 82 F. Ballistics performance values were within the specified requirements. The overall performance of the FSM-1 components and test equipment was nominal. Hughes, Phil D. Unspecified Center AMMONIUM PERCHLORATES; FULL SCALE TESTS; SOLID PROPELLANT ROCKET ENGINES; SPACE SHUTTLES; SPACE TRANSPORTATION SYSTEM FLIGHTS; STATIC TESTS; TEST FIRING; AMBIENT TEMPERATURE; BALLISTICS; INSPECTION; MANUFACTURING; QUALIFICATIONS...
Author : Carlton L. Horine,E. W. Madison
Publisher : Unknown
Page : 96 pages
File Size : 53,9 Mb
Release : 1971
Category : Solid propellant rockets
ISBN : CORNELL:31924003988551
Author : National Aeronautics and Space Adm Nasa
Publisher : Independently Published
Page : 64 pages
File Size : 50,9 Mb
Release : 2018-11-06
Category : Science
ISBN : 1730879683
The STS-78 Space Shuttle Program Mission Report summarizes the Payload activities as well as the Orbiter, External Tank (ET), Solid Rocket Booster (SRB), Reusable Solid Rocket Motor (RSRM), and the Space Shuttle main engine (SSME) systems performance during the seventy-eighth flight of the Space Shuttle Program, the fifty-third flight since the return-to-flight, and the twentieth flight of the Orbiter Columbia (OV-102). In addition to the Orbiter, the flight vehicle consisted of an ET that was designated ET-79; three SSME's that were designated as serial numbers 2041, 2039, and 2036 in positions 1, 2, and 3, respectively; and two SRB's that were designated BI-081. The RSRM's, designated RSRM-55, were installed in each SRB and the individual RSRM's were designated as 360L055A for the left SRB, and 360L055B for the right SRB. The STS-78 Space Shuttle Program Mission Report fulfills the Space Shuttle Program requirement as documented in NSTS 07700, Volume 7, Appendix E. The requirement stated in that document is that each organizational element supporting the Program will report the results of their hardware (and software) evaluation and mission performance plus identify all related in-flight anomalies. The primary objective of this flight was to successfully perform the planned operations of the Life and Microgravity Spacelab experiments. The secondary objectives of this flight were to complete the operations of the Orbital Acceleration Research Experiment (OARE), Biological Research in Canister Unit-Block II (BRIC), and the Shuttle Amateur Radio Experiment II-Configuration C (SAREX-II). The STS-78 mission was planned as a 16-day, plus one day flight plus two contingency days, which were available for weather avoidance or Orbiter contingency operations. The sequence of events for the STS-78 mission is shown in Table 1, and the Space Shuttle Vehicle Management Office Problem Tracking List is shown in Table 2. The Government Furnished Equipment/Flight Crew Equipment (GF...
Author : William H. Miller
Publisher : Unknown
Page : 124 pages
File Size : 52,6 Mb
Release : 1971
Category : Solid propellant rockets
ISBN : NASA:31769000661085
Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 142 pages
File Size : 45,6 Mb
Release : 1991
Category : Space sciences
ISBN : MINN:30000002622474
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 166 pages
File Size : 51,9 Mb
Release : 2018-07-17
Category : Electronic
ISBN : 1723079154
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 : United States. Congress. House. Committee on Science and Technology
Publisher : Unknown
Page : 604 pages
File Size : 40,6 Mb
Release : 1986
Category : Astronautics
ISBN : UCBK:B001166051
Author : United States. Congress. Senate. Committee on Commerce, Science, and Transportation
Publisher : Unknown
Page : 18 pages
File Size : 43,5 Mb
Release : 1989
Category : Rocketry
ISBN : OCLC:20113811
