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  • Educational brief : exploring Mars 
    Treiman, Allan H.; https://orcid.org/0000-0002-8073-2839; Kiefer, Walter S.; https://orcid.org/0000-0001-6741-5460 (National Aeronautics and Space Administration, 1999-01)
    A NASA Educational Brief on Mars exploration.
  • Educational brief : exploring Mars 
    Treiman, Allan H.; https://orcid.org/0000-0002-8073-2839; Kiefer, Walter S.; https://orcid.org/0000-0001-6741-5460 (National Aeronautics and Space Administration, 2002-09)
    A NASA Educational Brief on Mars exploration. For educators of grades 5-12.
  • EEE parts list for the LEAM Experiment 
    Van Hoorde, G. R. (Bendix Aerospace Systems Division, 1971)
    Presented herein is a composite list of EEE parts used in the LEAM experiment. Section A presents LEAM Bendix EEE parts list. Section B presents LEAM Time Zero EEE parts list.
  • EEE parts list for the LSG Experiments 
    Van Hoorde, G. R. (Bendix Aerospace Systems Division, 1971)
    Presented herein is the composite list of EEE parts used in the LSG experiment.
  • Effect of North and South Hadley Rille Landing Sites on ALSEP Array A-2 thermal performance 
    Urbanik, R. (Bendix Aerospace Systems Division, 1971)
    Presented herein are the results of a brief study conducted to evaluate the effect on the ALSEP Array A-2 thermal performance by the lunar terrain surrounding the two candidate Hadley Rille landing sites.
  • The Effect of Ocean Loading on the Growth of Basaltic Ocean Island Volcanoes and Their Magmatic Plumbing System 
    Le Corvec, Nicolas Le; McGovern, Patrick J. (Geophysicist); https://orcid.org/0000-0001-9647-3096 (2018-09-07)
    Basaltic shield volcanoes most commonly form as intraplate volcanic ocean islands that arise from the ocean floor and continue to grow above the sea water level to form gigantic volcanic edifices. The volcanic edifice ...
  • Effects of lift force on ejecta transport 
    Pai, S. I.; Menon, S.; Schultz, Peter H., 1944- (Pergamon Press, 1979)
    The possible effects of lift on individual ejecta trajectories after an impact event are examined, considering a dimensionless transport parameter (K), the initial velocity vector of the particles, and the ratio of the ...
  • Effects of the Lunar Module on ALSEP. 
    Unknown author (Bendix Aerospace Systems Division, 1967)
    Attached is a copy of a memo generated by Space Physics Division of MSC further confirming that the LM assent over pressure effects should not affect ALSEP, flying debris is negligible, and it is unlikely that LM will explode.
  • Eighth Huntsville Gamma-Ray Burst Symposium : October 24–28, 2016, Huntsville, Alabama 
    Connaughton, Valerie; Goldstein, Adam; https://orcid.org/0000-0002-0587-7042; Gehrels, Neil (Lunar and Planetary Institute, 2016)
    The Eighth Huntsville Gamma-Ray Burst Symposium will cover all areas of GRB science with a particular emphasis on multi-messenger observations and theory. Topics will include prompt emission (observations and theory), ...
  • The Eighth International Conference on Mars 
    Beaty, D. W. (David W.); Ehlmann, Bethany; McCleese, Daniel J.; Meyer, Michael (Planetary scientist); Zurek, Richard William, 1947- (Lunar and Planetary Institute, 2014)
    The Eighth International Mars Conference will be an ideal time to step back and summarize our current understanding of Mars, consolidate our primary paradigms for martian processes and history, and refocus the primary ...
  • Electronic systems test program ALSEP (Array E) STDN USB compatibility test report 
    Logan, Joseph C. (Manned Spacecraft Center, 1972)
    This document presents the objectives, results, and conclusions of the ALSEP (Array E) Spaceflight Tracking and Data Network (STDN) Unified S-band (USB) Compatibility Test Program. The tests were performed in the Electronic: ...
  • Electronic systems test program Apollo communications system ALSEP command link test report 
    Patrick, A. E.; Logan, Joseph C. (Lockheed Electronics Company, Houston Aerospace Systems Division, 1969)
    To verify the command link from the unified S-band Manned Space Flight Network (MSFN) to the Apollo Lunar Surface Experiments Package (ALSEP), a series of tests was performed at the Manned Spacecraft Center at Houston, ...
  • EMI investigation for Array E 
    Jensen, C. W. (Bendix Aerospace Systems Division, 1971)
    This ATM documents the results of an investigation of the Electromagnetic Compatibility (EMC) of the ALSEP Array E (Apollo 17) System. The basic EMC requirements are first established, an analysis is included to show that ...
  • EMI protection design guideline 
    Whiteford, James E.; Lewis, L. R. (Bendix Systems Division, 1966)
    This EMI Protection Design Guidelines report has been prepared as a guide for use by ALSEP experiment fabrication and subsystem designers.
  • EMI test results and margin of compatibility for ALSEP Array E 
    Cripps, G. A. (Bendix Aerospace Systems Division, 1972)
    This ATM provides an overall assessment of the EMI characteristics of the Flight 6 ALSEP System and summarizes the results of the Flight and Qualification Test Programs relative to EMI capability.
  • Enceladus and the Icy Moons of Saturn : July 26-29, 2016, Boulder, Colorado 
    Esposito, Larry; Howett, Carly J. A.; Bloom, Laura; Schenk, Paul M. (Lunar and Planetary Institute, 2016)
    Topics include (but are not limited to) geology, geophysics, geochemistry and mineralogy, active jets and their properties and origins, formation and evolution, astrobiology, and future investigations of these bodies. ...
  • End item specification for the LRRR (300) crew training model 
    Marrus, Leslie D. (Bendix Aerospace Systems Division, 1970)
    This specification defines the performance, design, construction, and interface requirements for the Crew Training Model of the Laser Ranging Retro-Reflector (LRRR). This model is a mechanical simulation of the LRRR (300) ...
  • Engineering study program to determine the optimum design for a hand held camera to be used on the lunar surface 
    Unknown author (Goerz Optical Company, Inc., 1965-06-04)
    The purpose of this study was to determine the optimum design for a hand held stereo camera considering the types of data to be taken, the environmental conditions, the limited dexterity of the space suited astronaut and ...
  • Engineering study program to determine the optimum design for a hand-held camera to be used on the lunar surface, mid-term report 
    Unknown author (C. P. Goerz American Optical, 1965)
    During the first two months, materials were selected and the design of a high resolution, wide spectral range lens was carried nearly to completion. An investigation of requirements for artificial illumination showed the ...
  • Equipment constraints on ALSEP deployment sequence 
    Neau, O. T. (Bendix Aerospace Systems Division, 1968)
    The major equipment constraints on the ALSEP deployment sequence are defined and basic background material for the constraints is presented.

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