Optimized cost/performance design methodology. Volume 2 - Data review and analysis. Book 1 - Design
Mission requirements and physical and functional characteristics for optimized cost orbital space transportation system design
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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A Study of 30 Km to 200 Km Meteorological Rocket Sounding Systems, Volume 1. Part 2 - Literature and Data Review
Analysis of current meteorological rocket sounding systems for 30 km to 200 km region
Bollerman, B.↗
A Study of 30 Km to 200 Km Meteorological Rocket Sounding Systems, Volume 1, Part 1 - Literature and Data Review
Literature review on meteorological rockets and system requirements and techniques for upper atmosphere sounding
Bollerman, B.↗
Ocmulgee national monument visitor center solar heating and cooling system design review data
The design of a solar heating and cooling system is documented. Solar collectors, design approaches, system trade studies, and preliminary specifications are discussed.
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Thematic mapper flight model preshipment review data package. Volume 2, part A: Subsystem data
Performance and acceptance data are presented for the multiplexer, scan mirror, power supply, mainframe/top mechanical and the aft optics, assemblies. Other major subsystems evaluated include the relay optics, the electronic module, the radiative cooler, and the cable harness. Reference lists of nonconforming materials reports, failure reports, and requests for deviation/waiver are also given.
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Thematic mapper flight model preshipment review data package. Volume 2, part B: Subsystem data
Summarized performance data are presented for the following major subsystems of the thematic mapper: the focal plane assembly, the radiative cooler, the radiative cooler door assembly, the top optical assembly, and the telescope assembly. Reference lists of the configurations status and of nonconforming material reports, failure reports, and requests for deviation/waiver are included.
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Thematic mapper flight model preshipment review data package. Volume 2, part C: Subsystem data
Reference lists are provided to acceptance data for each of the major subsystems of the thematic mapper. Configuration reports, lists and copies of all failure reports, and requests for deviation/waiver are included.
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Thematic mapper flight model preshipment review data package. Volume 3, part A: System data
Results of vibration, acoustical noise, and thermal vacuum are described as well as tests studies of EMI/EMC and mass properties conducted for thematic mapper systems integration. Liens are summarized and the engineering change proposal status is presented. Requests for deviation/waiver are included along with failure and nonforming material reports.
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Thematic mapper flight model preshipment review data package. Volume 3, part B: System data
Procedures and results are presented for performance and systems integration tests of flight model-1 thematic mapper. Aspects considered cover electronic module integration, radiometric calibration, spectral matching, spatial coverage, radiometric calibration of the calibrator, coherent noise, dynamic square wave response, band to band registration, geometric accuracy, and self induced vibration. Thermal vacuum tests, EMI/EMS, and mass properties are included. Liens are summarized.
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Thematic mapper flight model preshipment review data package. Volume 3, part C: System data
Failure reports for flight model-1 of the thematic mapper are summarized showing the symptom and cause of failure as well as the corrective action taken. Each report is keyed to the major subsystem against which the failure occurred. Requests for deviation/waiver are listed by number, description, and current status. Copies of engineering proposals are included.
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Thematic mapper protoflight model preshipment review data package. Volume 4: Appendix. Part A: Multiplexer data, book 1
Data from the final performance tests of the thematic mapper flight model multiplexer at ambient temperature are presented. Results cover the power supply, the input buffer, and the A/D threshold for bands 1 through 4.
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Thematic mapper protoflight model preshipment review data package. Volume 4: Appendix. Part A: Multiplexer data book 2
Final performance test data for the thematic mapper flight model multiplexer are presented in tables. Aspects covered include A/D thresholds for bands 5, 6, and 7; cross talk; the thermistor; bilevel commands signal parameters; A/D threshold ambient, voltage margin low bus; serial data and bit clock parameters; and the wire check. Tests were conducted at ambient temperature.
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Thematic mapper flight model preshipment review data package. Volume 4: Appendix. Part B: Scan mirror assembly data
Data from the thematic mapper scan mirror assembly (SMA) acceptance test are presented. Documentation includes: (1) a list of the acceptance test discrepancies; (2) flight 1 SMA test data book; (3) flight 1 SMA environmental report; (4) the configuration verification index; (5) the flight 1 SMA test failure reports; (6) the flight 1 data tapes log; and (7) the requests for deviation/waivers.
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Thematic mapper flight model preshipment review data package. Volume 4: Appendix. Part D: Focal plane assembly data
The data obtained for the Band 1 thematic mapper flight full band assembly (P/N 50797) are summarized. The data were collected from half band, post amplifier, and full band acceptance test data records.
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Thematic mapper flight model preshipment review data package. Volume 4: Appendix. Part E: Electronics module data
Tests to verify the as-designed performance of all circuits within the thematic mapper electronics module unit are described. Specifically, the tests involved the evaluation of the scan line corrector driver, shutter drivers function, cal lamp controller function, post amplifier function, command decoder verification unit, and the temperature and actuator controllers function.
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Thematic mapper flight model preshipment review data package. Volume 4: Appendix. Part F: Radiative cooler
Performance data for the thematic mapper radiative cooler are presented. Results from workmanship vibration tests and thermal vacuum test are described and an assembly history record is given.
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Thematic mapper flight model preshipment review data package. Volume 4: Appendix. Part G: Miscellaneous system data
Functional and design data from various thematic mapper subsystems are presented. Coarse focus, modulation transfer function, and shim requirements are addressed along with spectral matching and spatial coverage tests.
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Radial SI latches vibration test data review
Dynamic testing of the Space Telescope Scientific Instrument Radial Latches was performed as specified by the designated test criteria. No structural failures were observed during the test. The alignment stability of the instrument simulator was within required tolerances after testing. Particulates were discovered around the latch bases, after testing, due to wearing at the B and C latch interface surfaces. This report covers criteria derivation, testing, and test results.
Harrison, P. M.↗