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  • 1
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    Gemini Program features and results (1966)
    In:  CASI
    Details
    Publication Date: 2006-10-26
    Description: Systems design, mission operations, overall results, and applications to future space programs of Gemini project findings
    Keywords: SPACE VEHICLES
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    Design principles stressing simplicity (1970)
    In:  Other Sources
    Details
    Publication Date: 2011-08-16
    Description: Apollo project hardware design and evaluation principles coupling simple design practice with stringent technical and administrative discipline
    Keywords: SPACE VEHICLES
    Type: ; DIOTEKHNIKA (
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    Project Review (1963)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: Review of mercury project
    Keywords: STRUCTURAL MECHANICS
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 4
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    Systems design experience from three manned space programs. (1969)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Systems design experience derived from Mercury, Gemini and Apollo projects, discussing thermal protection, launch propulsion, life support, etc
    Keywords: SPACE VEHICLES
    Type: AIAA PAPER 69-1077 , AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ANNUAL MEETING AND TECHNICAL DISPLAY, 6TH; Oct 20, 1969 - Oct 24, 1969; ANAHEIM, CA
    Format: text
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    NASA TECHNICAL REPORTS
  • 5
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    Skylab student project. (1972)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Review of the Skylab student project conceived to stimulate interest in science and technology by directly involving students in a major research program. Under this project, over 4000 students, ranging in age from 11 to 19 years, submitted proposals from which 301 regional winners and, then, 25 national winners were selected on the basis of their scientific and technical merits. Descriptions are presented of the proposal of these 25 national winners.
    Keywords: GENERAL
    Type: International Astronautical Federation, International Astronautical Congress; Oct 08, 1972 - Oct 15, 1972; Vienna; Austria
    Format: text
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    NASA TECHNICAL REPORTS
  • 6
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    Skylab rescue capability. (1972)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Skylab is an experimental manned space station scheduled to be placed into orbit in 1973. The Skylab system is to provide support for occupancy by a three-man crew for a total of up to five months. After an extensive study of various means by which rescue capability could be provided for Skylab, a plan was devised that provides coverage for those situations which are the most likely to arise. Rescue mission requirements are discussed together with a response-time analysis and the rescue vehicle configuration. The time-to-rescue will vary from 48 to 10 days, depending on the launch-readiness state at the time of a mission emergency.
    Keywords: SPACE VEHICLES
    Type: International Astronautical Federation, International Astronautical Congress; Oct 08, 1972 - Oct 15, 1972; Vienna; Austria
    Format: text
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    NASA TECHNICAL REPORTS
  • 7
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    United States manned spacecraft reliability experience (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-07-27
    Description: Attention is given to the reliability controls in manned spacecraft programs, taking into account the project Mercury, the Gemini program, the Apollo program, the Skylab program, and the Apollo-Soyuz test project. Reliability controls used in these programs are related to reliability management, parts and materials control, failure mode and effects analysis, reliability quantitative analysis, problem reporting and corrective action control, test control, limited-life control, and milestone reviews. A summary is presented of the major reliability tasks and innovations being used on the Space Shuttle program. Examples of these innovations include improved management techniques and an early identification of specific certification tests.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: IAF PAPER 74-049
    Format: text
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    NASA TECHNICAL REPORTS
  • 8
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    System safety as applied to Skylab (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-07-27
    Description: Procedural and organizational guidelines used in accordance with NASA safety policy for the Skylab missions are outlined. The basic areas examined in the safety program for Skylab were the crew interface, extra-vehicular activity (EVA), energy sources, spacecraft interface, and hardware complexity. Fire prevention was a primary goal, with firefighting as backup. Studies of the vectorcardiogram and sleep monitoring experiments exemplify special efforts to prevent fire and shock. The final fire control study included material review, fire detection capability, and fire extinguishing capability. Contractors had major responsibility for system safety. Failure mode and effects analysis (FMEA) and equipment criticality categories are outlined. Redundancy was provided on systems that were critical to crew survival (category I). The five key checkpoints in Skylab hardware development are explained. Skylab rescue capability was demonstrated by preparations to rescue the Skylab 3 crew after their spacecraft developed attitude control problems.
    Keywords: LAUNCH VEHICLES AND SPACE VEHICLES
    Type: IAF PAPER A74-33
    Format: text
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    NASA TECHNICAL REPORTS
  • 9
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    Systems design experience from three manned space programs (1970)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Systems design experience derived from Mercury Gemini and Apollo projects, discussing thermal protection, launch propulsion, life support, etc
    Keywords: SPACE VEHICLES
    Type: AIAA PAPER 69-1077 , AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ANNUAL MEETING AND TECHNICAL DISPLAY, 6TH; Oct 20, 1969 - Oct 24, 1969; ANAHEIM, CA|; STITUTION OF ENGINEE
    Format: text
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    NASA TECHNICAL REPORTS
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