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  • 1
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    Apollo 13 Case Study Part 1 and 2 (2008)
    In:  CASI
    Details
    Publication Date: 2018-06-11
    Description: Objectives: a) Describe the Service Module Electrical Power System hardware; b) Describe the circumstances which led to the Apollo 13 accident c) Summarize the Mission Control and crew reaction.
    Keywords: Spacecraft Design, Testing and Performance
    Type: Apollo 13 Blu Ray DVD
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 2
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    CSM RCS Design Considerations and Failure Modes (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: Objectives include: a) Define major Command and Service Module (CSM) design considerations; b) List Command Module (CM) RCS failures and lessons learned; and c) List Service Module (SM) RCS failures and lessons learned.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-17237-7
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    Saturn V - Design Considerations and Launch Issues (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: Objectives include: a) Understand some of the design considerations that went into creating the Saturn V launch vehicle; b) Gain an appreciation for some of the manufacturing issues concerning the Saturn V; and c) Review three major problems that affected Saturn V launches.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-17237-22
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 4
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    Lunar Surface Operations (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: This slide presentation reviews the first part of the post-touchdown lunar surface and system checkout tasks. A stay/no stay decision for the lunar lander was made based on the questions: "Is the Lunar Module (LM) stable on the lunar surface?"; "Are there any time critical systems failures or trends indicating impending loss of capability to ascent and achieve a safe lunar orbit?"; and "Is there loss of capability in critical LM systems?" The sequence of these decisions is given as a time after touchdown on the surface of the moon. After the decision to stay is made the next task is to checkout status of the lunar module. While the status of the lunar module is checking out certain conditions, the Command Service Module was also engaged in certain checkout activities.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-17237-19
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    Saturn V Stage I (S-IC) Overview (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: Objectives include: a) Become familiar with the Saturn V Stage I (S-IC) major structural components: Forward Skirt, Oxidizer Tank, Intertank, Fuel Tank, and Thrust Structure. b) Gain a general understanding of the Stage I subsystems: Fuel, Oxidizer, Instrumentation, Flight Control, Environmental Control, Electrical, Control Pressure, and Ordinance.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-17237-24
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
  • 6
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    Apollo Lunar Module Electrical Power System Overview (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: Objectives include: a) Describe LM Electrical System original specifications; b) Describe the decision to change from fuel cells to batteries and other changes; c) Describe the Electrical system; and d) Describe the Apollo 13 failure from the LM perspective.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-17237-17
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 7
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    Lunar Module ECS (Environmental Control System) - Design Considerations and Failure Modes (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: Design considerations and failure modes for the Lunar Module (LM) Environmental Control System (ECS) are described. An overview of the the oxygen supply and cabin pressurization, atmosphere revitalization, water management and heat transport systems are provided. Design considerations including reliability, flight instrumentation, modularization and the change to the use of batteries instead of fuel cells are discussed. A summary is provided for the LM ECS general testing regime.
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-17237-12 , Apollo 13 Blu Ray DVD and BD Live Server comment, January 2009
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 8
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    Lunar Module Environmental Control System Design Considerations and Failure Modes (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: This viewgraph presentation seeks to describe the Lunar Module Environmental Control System (ECS) subsystem testing and redesign and seeks to summarize the in-flight failures of the Lunar Module (LM) Environmental Control System (ECS).
    Keywords: Spacecraft Design, Testing and Performance
    Type: JSC-17237-11
    Format: application/pdf
    Location Call Number Expected Availability
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    NASA TECHNICAL REPORTS
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