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  • Life and Death in the Chicxulub Impact Crater: A Record of the Paleocene–Eocene Thermal Maximum 
    Smith, Vann; Warny, Sophie; Grice, Kliti; Schaefer, Bettina; Whalen, Michael T.; Vellekoop, Johan; Chenot, Elise; Gulick, Sean P. S.; Arenillas, Ignacio; Arz, Jose A.; Bauersachs, Thorsten; Bralower, Timothy J.; Demory, François; Gattacceca, Jérôme; Jones, Heather L.; Lofi, Johanna; Lowery, Christopher M.; Morgan, Joanna V.; Nuñez Otaño, Noelia B.; O'Keefe, Jennifer M. K.; O'Malley, Katherine; Rodríguez-Tovar, Francisco J.; Schwark, Lorenz; IODP-ICDP Expedition 364 Scientists (EGU Publications, 2020-10-19)
    Here, we present a new record of the Paleocene–Eocene Thermal Maximum (PETM) from the peak ring of the Chicxulub impact crater that has been identified based on nannofossil biostratigraphy, an acme of the dinoflagellate ...
  • Linearizing thermistors for use as temperature sensors 
    Steinmeye, D. R. (Bendix Corporation, Aerospace Systems Division, 1972)
    Conventional negative temperature coefficient thermistors can be made to give a linear emf readout over a limited range if used in the right kind of circuit. A computer program is described which, given the thermistor data ...
  • Lithification of vitric - and clastic-matrix breccias: SEM petrography 
    Phinney, William C.; Simonds, Charles H.; McKay, David S.; Warner, Jeffrey L. (Pergamon Press, 1976)
    Matrix textures of 41 lunar breccias ranging from very friable soil clods through coherent microbreccias and tough vitric breccias to tough, fine-grained crystalline breccias were examined petrographically by means of the ...
  • LMS experiment non metallic materials list 
    Howell, F. L.; Hiebert, Robert W. (Bendix Aerospace Systems Division, 1971)
    Presented herein is the Non Metallic Materials List for the LMS. Exhibit A defines Non Metallic Materials for BxA and Exhibit B defines Non Metallic Materials for UTD portions of the LMS design. The data herein represents ...
  • LMS qualification and flight acceptance T/V test summary and thermal design final report 
    Toelle, Dan. (Bendix Aerospace Systems Division, 1972)
    This ATM summarizes the analytical and test results of the Lunar Mass Spectrometer thermal control system. The first section introduces the hardware and develops the mathematical thermal model of the experiment. The second ...
  • LMS reliability EE parts list addendum -1 
    Hiebert, Robert W. (Bendix Aerospace Systems Division, 1971)
    This Addendum updates the subject ATM per request on NASA letter EH 2/l0-8/L503/l3-480.
  • LMS reliability FMECA and SPFS 
    Hiebert, Robert W. (Bendix Aerospace Systems Division, 1972)
    Presented herein are the Failure Mode Effects and Criticality Analysis and the Single Point Failure Summary for the Lunar Mass Spectrometer. The "A" Revision was required to include the Lock Out Switching Circuit(see page ...
  • LMS reliability part application analysis 
    Hiebert, Robert W. (Bendix Aerospace Systems Division, 1972)
    Presented herein are the parts application analysis results as performed on the Lunar Mass Spectrometer. Parts application analysis worksheets are presented in Appendix A for BxA and in Appendix B for UTD. The A Revision ...
  • LMS reliability time/cycle sensitive parts list 
    Hendrickson, J. E. (Bendix Aerospace Systems Division, 1972)
    The time/cycle sensitive parts for ALSEP Array E LMS experiment are shown below. These parts are the only ones which may be cycled to a degree in which the performance changes over a two year period.
  • LMS thermal/vacuum test reports 
    Tente, A. S. (Bendix Aerospace Systems Division, 1971)
    The compiled reports contained herein represent the total data accumulated in the testing of the LMS components in a simulated lunar environment.
  • lntracrystalline cation order in a lunar crustal troctolite 
    Smyth, J. R. (Pergamon Press, 1975)
    Lunar rock 76535 appears to be one of the most slowly cooled bits of silicate material yet studied. The crystal structures of its three major phases, anorthite, olivine, and bronzite have been refined from three-dimensional ...
  • Log of ALSEP technical memoranda (ATM). 
    Unknown author (Bendix Corporation Aerospace Systems Division?, 1966-1972)
    Gives the ATM number, issue date, author, and title for the ALSEP technical memoranda (ATM) from Bendix.
  • Long-term differential energy spectrum for solar-flare iron-group particles 
    Blanford, G. E.; Fruland, Ruth M.; Morrison, Donald A. (Pergamon Press, 1975)
    Track density profile measurements in sample 64455 and sample 68815 have been used to derive a long-term solar-flare differential energy spectrum for iron-group (20 ~ Z ~ 26) nuclei from --0.1 to --600 MeV/a.m.u.
  • Low-Cost Science Mission Concepts for Mars Exploration : March 29–31, 2022, Pasadena, California 
    Curry, Shannon M.; Banfield, Don J. (Lunar and Planetary Institute, 2022)
    Emerging small spacecraft capabilities and innovative new mission concepts offer opportunities for compelling science discoveries at Mars at unprecedented low costs. Here, "low-cost" equates to mission costs that fall well ...
  • LRRR (300) task sequence/timeline for Hadley Rille Landing Site 
    Marrus, Leslie D. (Bendix Aerospace Systems Division, 1971)
    The attached LRRR (300) Task Sequence/Timeline for the Hadley Rille Landing Site provides a basic description of the astronaut operations required to completely deploy the Apollo 15 configuration of the LRRR (300).
  • LRRR (300) task sequence/timeline for Hadley Rille Landing Site 
    Marrus, Leslie D. (Bendix Aerospace Systems Division, 1971)
    The attached LRRR (300) Task Sequence/Timeline for the Hadley Rille Landing Site provides a basic description of the astronaut operations required to completely deploy the Apollo 15 configuration of the LRRR (300).
  • LRRR 300 Corner Array dynamic analysis 
    Goran, M.; Min, G. B.; Wadleigh, K. H. (Bendix Aerospace Systems Division, 1971)
    This ATM presents the results of the structural dynamics analysis performed on the Lunar Ranging Retro Reflector 300 Corner Array.
  • LRRR 300 thermal design final report 
    Granholm, E. A. (Bendix Aerospace Systems Division, 1970)
    The results of thermal design/analyses performed on the 300 corner Laser Ranging Retro-Reflector (LRRR 300) to determine array operating temperature levels, net array/lunar environment heat exchange, and corner optical ...
  • LRRR astronaut trainer acceptance test results 
    Redick, Ronald L. (Bendix Aerospace Systems Division, 1970)
    This ATM reports the results of the Crew Systems and Operations Acceptance Test for the LRRR Astronaut Trainer.
  • LRRR emplacement range and azimuth from LM 
    Cornille, H. (Bendix Aerospace Systems Division, 1970)
    Potential damage to the LRRR could be caused by excessive heat, dust or kapton contamination of the retro-reflector faces, or physical movement of the LRRR which produces misalignment.

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