USRA Houston Repository

Browsing ALSEP Documents by Title

Browsing ALSEP Documents by Title

Sort by:Order:Results:

  • Bendix Aerospace Systems Division (Bendix Aerospace Systems Division., 1970)
    A non-technical review of the first year of ALSEP, left on the Moon by the Apollo 12 mission
  • Fox, T. W. (Bendix Aerospace Systems Division, 1972)
    On 14 July 1971 MSC issued an ALERT (MSC-71-04) on Texas Instruments 54L series integrated circuits. This ALERT indicated that devices manufactured prior to the second week of August 1971 may contain conductive particulate ...
  • Simmons, Gene, 1929- (Massachusetts Institute of Technology, 1972)
  • Unknown author (publisher unknown, 1970)
    Drawings depict ALSEP instruments and their use on the Moon.
  • Cooper, J. W. (Bendix Aerospace Systems Division, 1971)
    At PDR, NASA has asked BxA to re-examine the present reefing line/pyrotechnic squib plans to be sure they are optimized with respect to reliability and other pertinent engineering parameters.
  • Anthis, W. (Bendix Aerospace Systems Division, 1970)
    Parts and materials used in the Array are listed on sheets which reflect the three subassemblies of the array: A. Panel Structure Assembly B. Insulation Assembly C. Retro-Reflector Array Assembly.
  • Moskowitz, Lee S. (Bendix Aerospace Systems Division, 1970)
    Parts and materials used in the Array are listed on the attached sheets which reflect the three subassemblies of the array for the Apollo 14 Flight Unit: A. Panel Structure Assembly B. Insulation Assembly C. Retro-Reflector ...
  • Krause, P. (Bendix Aerospace Systems Division, 1967)
    This ATM discusses an alternate stowage design for the mortar box antenna cable.
  • Wallace, R. B. (Bendix, Aerospace Systems Division, 1973)
    At 0926 GMT (actual 0919 GMT) on 26 March 1973 Apollo 16 ALSEP transmitter B was selected by mission control. Switch over was implemented after a series of data dropouts, beginning 4 March 1973 and reported by several ...
  • Fox, T. W. (Bendix Aerospace Systems Division, 1970)
    This report presents a Failure Mode, Effects and Criticality Analysis (FMECA) performed on the Data Transmitter and documented in the attached worksheets.
  • Fox, T. W. (Bendix Aerospace Systems Division, 1970)
    This report presents the Data Transmitter reliability prediction estimates derived through the studies of Data Transmitter Failure Mode, Effects and Criticality Analysis (FMECA) and Data Transmitter Parts Application ...
  • Gilson, R. (Bendix Corporation, Aerospace Systems Division, 1971)
    Since 219/10/27/56 EGMT, data from A2 Heat Flow Experiment probe 2 thermocouple reference bridge Channel DH15 (DH91=1110) has exhibited symptoms that indicate a possible failure within the HFE electronics. At the above ...
  • Balsiger, H.; Freeman, John W.; Hills, H. Kent. (Department of Space Science, Rice University, 1970)
    An experiment designed to measure the differential energy spectrum and a coarse mass spectrum of ions near the lunar surface (Suprathermal Ion Detector Experiment) was deployed by the Apollo XII astronauts. This experiment ...
  • Sondeen, P. (Bendix Systems Division, 1966)
    This report contains a list of electronic common parts which are recommended for application in ALSEP equipment.
  • Liepa, L. V. (Bendix Aerospace Systems Division, 1967)
    The following is an analysis of the accuracy of redundant (Photographic) means of measuring grenade velocity as planned during ASE grenade firings at WSMR.
  • Bryer, Carl. (Bendix Systems Division, 1967)
    This ATM is written in response to an MSC request to document an analysis of grenade thrust beyond the launch tube.
  • Zimmer, J. (Bendix Systems Division, 1966)
    The engineering model test plan written by the Active Seismic Experiment Engineering Group. This outlines and describes the scope and objective of the test that will be made by the ASE Engineering Group with the engineering ...
  • Lanning, H. E. (Bendix Systems Division, 1966)
    This ATM determines the probability of sync, false sync, and the probability of loosing sync for an 11 bit and 6 bit frame sync code. The number of bits/frame range from 1344 to 4032. The amount of data lost during loss ...
  • Schmidt, R. A. (Bendix Systems Division, 1966)
    This ATM describes and compares three different word formats for the Active Seismic Experiment.
  • Redick, Ronald L. (Bendix Aerospace Systems Division, 1971)
    As a result of recent activities involving Boydbolts for A-2, an additional step in the crew procedures should be added in the event that a spindle does not depress.

Search HOU Repository


Browse

My Account