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  • 1
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    Apollo Lesson Sampler: Apollo 13 Lessons Learned (2008)
    In:  Other Sources
    Details
    Publication Date: 2018-06-11
    Description: This CD-ROM contains a two-part case study of the Apollo 13 accident. The first lesson contains an overview of the electrical system hardware on the Apollo spacecraft, providing a context for the details of the oxygen tank explosion, and the failure chain reconstruction that led to the conditions present at the time of the accident. Given this background, the lesson then covers the tank explosion and immediate damage to the spacecraft, and the immediate response of Mission Control to what they saw. Part 2 of the lesson picks up shortly after the explosion of the oxygen tank on Apollo 13, and discusses how Mission Control gained insight to and understanding of the damage in the aftermath. Impacts to various spacecraft systems are presented, along with Mission Control's reactions and plans for in-flight recovery leading to a successful entry. Finally, post-flight vehicle changes are presented along with the lessons learned.
    Keywords: Space Transportation and Safety
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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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
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    NASA TECHNICAL REPORTS
  • 3
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    CSM/LM Lighting (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: Objectives include: a)Identify the types and uses of the various lighting components: Interior (CM, LM), Exterior (CSM, LM); b) Explain the purpose and locations of electroluminescent (EL) and radioluminescent (RL)lighting techniques; c) Understand the use of various D&C lighting components; and d) Understand in-flight anomalies.
    Keywords: Optics
    Type: JSC-17237-9
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 4
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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
  • 5
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    Earth Parking Orbit and Translunar Injection (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: The objectives of this slide presentation are to (1) Describe the general characteristics of the Earth Parking Orbit (EPO) and Translunar Injection (TLI) (2) List the general activities that occurred during EPO (4) State what went into verifying a working Saturn IVB S-IVB IU and a CSM GNC (5) Differentiate between a Free-Return Trajectory vs. a Hybrid Non-Free-Return Trajectory (6) Identify the crew monitoring task during the TLI Burn and (7) Identify the abort modes in the event of severe systems problems during the TLI timeframe
    Keywords: Space Communications, Spacecraft Communications, Command and Tracking
    Type: JSC-17237-8
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 6
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    Lunar Surface Operations (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: The objectives of this slide presentation are to review the activities on the lunar surface during the stay. The objectives include (1) Summarize Lunar Module Basics emphasizing module layout and storage. (2) Identify the primary activities occurring during each of the lunar s urface timelines, (3) List the EVA Prep tasks, (4) Identify the EVA Objectives, (5) Identify the activities associated with Post EVA (6) Describe the lessons learned during both EVA and Non EVA activities. Included are overview drawings of the Lunar Roving Vehicle, pictures of the tools, and sample return containers. There are also time lines for the Apollo 11, and Apollo 12 through 14, Apollo 15, Apollo 16 and Apollo 17. Diagrams of the EVA suits are shown, including the Liquid Cooling Garment, and the Pressure Garment Assembly. The activity prior to the EVA are reviewed. The science mission assignments of each mission are viewed. The activities after the EVA are reviewed
    Keywords: Lunar and Planetary Science and Exploration
    Type: JSC-17237-25
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 7
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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
  • 8
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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
  • 9
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    Apollo Recovery Operations (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: Objectives include: a) Describe the organization of recovery force command and control and landing areas; b) Describe the function and timeline use of the Earth Landing System (ELS); c) Describe Stable 1 vs Stable 2 landing configurations and the function of the Command Module Uprighting System; d) Explain the activities of the helicopter and swimmer teams in egress and recovery of the crew; e)Explain the activities of the swimmer teams and primary recovery ship in recovery of the Command Module; and f) Describe several landing incidents that occurred during Apollo.
    Keywords: Space Transportation and Safety
    Type: JSC-17237-21
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 10
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    Sequential Events Control System (SECS) Overview (2009)
    In:  CASI
    Details
    Publication Date: 2019-07-12
    Description: This slide presentation will cover the Sequential Events Control System (SECS), which is the Apollo spacecraft subsystem that controls the automatically sequenced functions during the mission and during any a borts that could be performed. Included in this presentation are its general architecture, its integration into and use of the spacecraft' s other systems, and details on the functions it is responsible for c ontrolling during the mission. The objectives are to describe the system's architecture, the major components in the system, and the major system functions.
    Keywords: Space Transportation and Safety
    Type: JSC-17237-23
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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