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Lunar Reconnaissance Orbiter (LRO) SRR/Mechanical System August 16-18, 2005

Lunar Reconnaissance Orbiter (LRO) SRR/Mechanical System August 16-18, 2005. Giulio.G.Rosanova@nasa.gov 301-286-5907 . Lunar Reconnaissance Orbiter (LRO) Mechanical System Applicable Documents. 431-RQMT-000004 LRO Requirements Document

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Lunar Reconnaissance Orbiter (LRO) SRR/Mechanical System August 16-18, 2005

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  1. Lunar Reconnaissance Orbiter (LRO)SRR/Mechanical SystemAugust 16-18, 2005 Giulio.G.Rosanova@nasa.gov 301-286-5907

  2. Lunar Reconnaissance Orbiter (LRO)Mechanical System Applicable Documents 431-RQMT-000004 LRO Requirements Document 430-PG-1410.2.1 Robotic Lunar Exploration Program Configuration Management Procedure 430-RQMT-000006 Robotic Lunar Exploration Program Mission Assurance Requirements Document 431-ANYS-000010 Radiation Analysis for the Lunar Reconnaissance Orbiter 431-PLAN-000005 LRO Systems Engineering Management Plan 431-PLAN-000110 LRO Contamination Control Plan 431-SPEC-000008 Electrical Systems Specification 431-SPEC-000012 LRO Mechanical Systems Specification 431-SPEC-000091 LRO Thermal Systems Specification 431-SPEC-000112 LRO Technical Resource Allocation Specification 431-SPEC-000113 LRO Pointing and Alignment Specification (ALL) LRO Instrument Mechanical Interface Control Documents (ALL) LRO Spacecraft Component Mechanical Interface Control Documents

  3. Lunar Reconnaissance Orbiter (LRO)Mechanical SystemLevel 2 Flow Down Key Requirements

  4. Lunar Reconnaissance Orbiter (LRO)Mechanical SystemLevel 2 Flow Down Key Requirements

  5. Lunar Reconnaissance Orbiter (LRO)Mechanical Concept ADDITIONAL VIEWS TO FOLLOW

  6. Lunar Reconnaissance Orbiter (LRO)Mechanical Verification Summary • Verify all Mechanical / Structural Designs and Functionality • Analysis • Comply with LRO General Structural-Thermal Environments, Interface, and Veification Requirements • Overall System Level Verification Matrix • Verification by Analysis, and or Verification by Test of Proto-Type and/or Proto-Flight Units • Facilitate Functional and Performance testing of the LRO Observatory • S/A & HGA Deployment Monitoring (Potentiometers) • S/A & HGA shall Survive in Deployed Position Immediately after Observatory Separation thru LTO • Qualification Testing • Mech System • Orbiter • Functional Testing • Life Tests • Deployment testing in T/V

  7. Lunar Reconnaissance Orbiter (LRO)Mechanical Requirements Summary • Mechanical System is ready to proceed to PDR

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