Add to ORKGThis ATM presents the results of the dynamic analysis and testing performed on the DVT model of the LEAM Experiment Package. The interface of this package is with the Array E (Apollo 17) - Subpack No. 2 pallet.prepared by L. Kaliniec, K. Wadleigh.Introduction and summary -- Analysis model -- Method of analysis and input levels -- Computed responses and test results -- Future efforts -- Dynamic loads and displacement
This revision of ATM 927 presents the results of parametric studies accomplished from 12/1/70 thru 1...
The Array E Subpackage No. 2 engineering model (EEM-SP2) was subjected to the ALSEP specified design...
An analysis of the Array E (Apollo 17) Central Station-LEAM digital interface was made.prepared by R...
This ATM gives the results of the dynamic analysis on the LEAM Flight Model Experiment Package. The ...
A functional test of the mechanical features used for release of folding mechanisms and deployment o...
This ATM documents the Failure Mode Effect and Criticality Analysis of the LEAM experiment. The anal...
This ATM summarizes the LEAM thermal control design, analysis and test program including the DVT T/V...
The LEAM DVT Thermal tests were conducted 15 March through 23 March 1971 in the NRC 4' x 8' thermal ...
The purpose of this ATM is to document the results of the parts application analysis study performed...
The Lunar Ejecta and Meteorites Experiment (LEAM) thermal design is a result of thermal math model d...
This ATM describes the transient analysis of ALSEP (E-1 Model) when subject to the LEM-ALSEP trapezo...
This ATM documents the Failure Modes, Effects and Criticality Analysis on the Lunar Seismic Profilin...
An investigation was conducted to determine why the temperature of the Lunar Ejecta and Meteorites E...
This technical memorandum represents the engineering vibration test report for EEM Subpackage No. 1 ...
Presented herein are the results of the reliability analysis conducted on the LEAM. This ATM compris...
This revision of ATM 927 presents the results of parametric studies accomplished from 12/1/70 thru 1...
The Array E Subpackage No. 2 engineering model (EEM-SP2) was subjected to the ALSEP specified design...
An analysis of the Array E (Apollo 17) Central Station-LEAM digital interface was made.prepared by R...
This ATM gives the results of the dynamic analysis on the LEAM Flight Model Experiment Package. The ...
A functional test of the mechanical features used for release of folding mechanisms and deployment o...
This ATM documents the Failure Mode Effect and Criticality Analysis of the LEAM experiment. The anal...
This ATM summarizes the LEAM thermal control design, analysis and test program including the DVT T/V...
The LEAM DVT Thermal tests were conducted 15 March through 23 March 1971 in the NRC 4' x 8' thermal ...
The purpose of this ATM is to document the results of the parts application analysis study performed...
The Lunar Ejecta and Meteorites Experiment (LEAM) thermal design is a result of thermal math model d...
This ATM describes the transient analysis of ALSEP (E-1 Model) when subject to the LEM-ALSEP trapezo...
This ATM documents the Failure Modes, Effects and Criticality Analysis on the Lunar Seismic Profilin...
An investigation was conducted to determine why the temperature of the Lunar Ejecta and Meteorites E...
This technical memorandum represents the engineering vibration test report for EEM Subpackage No. 1 ...
Presented herein are the results of the reliability analysis conducted on the LEAM. This ATM compris...
This revision of ATM 927 presents the results of parametric studies accomplished from 12/1/70 thru 1...
The Array E Subpackage No. 2 engineering model (EEM-SP2) was subjected to the ALSEP specified design...
An analysis of the Array E (Apollo 17) Central Station-LEAM digital interface was made.prepared by R...