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  • SPACE VEHICLES  (327)
  • 1970-1974  (327)
  • 1974  (327)
  • 1
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    Space shuttle (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: The space shuttle is discussed as a reusable space vehicle operated as a transportation system for space missions in low earth orbit. Space shuttle studies and operational capabilities are reported for potential missions indicating that about 38 percent are likely to be spacelab missions with the remainder being the replacement, revisit, or retrieval of automated spacecraft.
    Keywords: SPACE VEHICLES
    Type: NASA-TM-X-70384 , REPT-74-267
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    Apollo Soyuz test project. USA-USSR, fact sheet (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: The Apollo Soyuz Test Project (ASTP) is discussed. The United States and the Soviet Union have agreed to develop compatible rendezvous and docking systems which will provide a basis for docking and rescue on future spacecraft of both nations. The ASTP mission will include testing the rendezvous system in orbit, verifying techniques for transfer of astronauts and cosmonauts, and conducting experiments while docked and undocked. Diagrams of the spacecraft and systems involved in the tests are presented. The prime contractors for the equipment are identified. Biographical data on the astronauts participating in the program are provided.
    Keywords: SPACE VEHICLES
    Type: NASA-NEWS-RELEASE-74-196
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    First geosynchronous weather satellite prepared for launch (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: The Synchronous Meteorological Satellite (SMS), which is scheduled for launch 16 May 1974 is described along with the data transmission system. The Carrier Balloon System is discussed. The primary type of data to be obtained in conjunction with SMS and Nimbus F are meteorological, oceanographic, seismic, and tsunami information. The Space Environment Monitoring System is also described.
    Keywords: SPACE VEHICLES
    Type: NASA-NEWS-RELEASE-74-95
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 4
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    Wind Tunnel Test Results of Fairings on A.004 Scale Model Rockwell Space Shuttle Integrated Vehicle Aerodynamic Characteristics at Mach Numbers from 0.6 to 4.96 (IA62F) (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-14
    Description: Experimental aerodynamic investigations were conducted on a .004 scale model (34-OTS) orbiter, external tank, and solid rocket booster combined as an integrated vehicle in the NASA/MSFC 14 x 14 inch trisonic wind tunnel. The primary test objective was to determine the effect of a full length orbiter/external tank fairing on axial force. Secondary objectives were to define the static stability characteristics of the mated vehicle configuration with fairings over a Mach number range of 0.6 thru 4.96. Six component aerodynamic force and moment data were recorded over an angle of attack range from -10 deg to 10 deg at 0 deg sideslip angle and from -10 deg to 10 deg sideslip range at 0 deg and 5 deg angle of attack. Plotted and tabular results are presented herein.
    Keywords: SPACE VEHICLES
    Type: NASA-CR-134094 , DMS-DR-2103
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    The Space Shuttle Program and its technology (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-08-13
    Description: Review of the considerations leading to the development of the Space Shuttle system, followed by a description of the system and an analysis of the current program development status. The Space Shuttle system arose out of a need for a reusable vehicle that could routinely carry large payloads (up to 65,000 lb) into earth orbit and return on a cost-effective basis. The system, as currently baselined, consists of a manned reusable Orbiter vehicle and the booster hardware for ground launching. The proposed Orbiter will be 123 feet long, double delta-winged, and roughly the size of a DC-9. The Orbiter will normally carry a crew of four who will work without space suits in a shirtsleeve environment. The Orbiter will be boosted into space through the simultaneous operation of two solid propellant booster rockets and the Orbiter's three high-pressure liquid oxygen/liquid hydrogen main engines. The Orbiter will have reusable external insulation, since each vehicle will have a design life of ten years.
    Keywords: SPACE VEHICLES
    Type: Annual Meeting of the International Congress of Space Benefits; Jun 19, 1973 - Jun 20, 1973; Dallas, TX
    Format: text
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    NASA TECHNICAL REPORTS
  • 6
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    Saving Skylab (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-08-13
    Description: Initial difficulties encountered with the launch and operational deployment of the Skylab vehicle are described in terms of early indications of hardware failures, ground-based efforts at diagnosing the nature and significance of damage, and organization of improvized means and procedures for repair operations. Attention is given to heating and power-supply problems stemming from the loss of a micrometeoroid shield and a solar cell array. Systems engineering problems arising from the necessity of achieving a compromise among thermal, electrical, and stabilization requirements are explained, and repair solutions and operations in space and on the ground are described in detail.-
    Keywords: SPACE VEHICLES
    Type: Technology Review; 76; Jan. 197
    Format: text
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    NASA TECHNICAL REPORTS
  • 7
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    LST: The National Space Observatory concept - An observatory for future astronomer involvement in planning and use (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-08-13
    Description: The Large Space Telescope (LST) will be a unique facility which must be designed to serve the needs of all potential users throughout the world. This requires that a representative group of astronomers work intimately with the engineers in the early design of the telescope and that astronomers continue to be closely involved in the planning throughout the life of the project. Forty scientists are now defining the auxiliary instruments and their operation. Later, others will build instruments and participate in assigning observing time on the telescope, on the basis of the scientific merit of the proposed observation.
    Keywords: SPACE VEHICLES
    Type: Aerospace Sciences Meeting; Jan 30, 1974 - Feb 01, 1974; Washington, DC
    Format: text
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    NASA TECHNICAL REPORTS
  • 8
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    ATS-F spacecraft - An EMC challenge (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The Applications Technology Satellite F (ATS-F) is the latest of a series of satellites for communications, scientific experiments, and data collection. The physical configuration of the spacecraft is examined along with operational characteristics and EMC management and control. Predicted and encountered problems are discussed, giving attention to wiring pick-up and reradiation, input rectification and bias off-set, intermodulation products, harmonics, component degradation, electroexplosive devices, spacecraft test complex vulnerability, and launch environment testing. Approaches used for locating the problems are considered and a description is given of the key factors and constraints in achieving EMC.
    Keywords: SPACE VEHICLES
    Type: Electromagnetic Compatibility Symposium; Jul 16, 1974 - Jul 18, 1974; San Francisco, CA
    Format: text
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    NASA TECHNICAL REPORTS
  • 9
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    Design and performance of Skylab thermal/environmental control system (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: The function of the thermal/environmental control systems was to provide a comfortable thermal environment for the crew, to cool electronic components, to supply a controlled oxygen/nitrogen atmosphere, and to remove moisture, carbon dioxide, odors, and trace contaminants from the atmosphere. A separate refrigeration system was used to chill and freeze food and biomedical samples and to provide cold water for drinking. This paper describes system design and compares in-flight performance to preflight predictions. A discussion of in-flight anomalies and corrective actions is also included.
    Keywords: SPACE VEHICLES
    Type: AAS PAPER 74-127 , Annual Meeting; Aug 20, 1974 - Aug 22, 1974; Los Angeles, CA
    Format: text
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    NASA TECHNICAL REPORTS
  • 10
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    Flightcrew observations of spacecraft systems (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: A brief overview of the various Skylab systems is presented. Particular emphasis is placed on unique points of system design that were either new to space flight or had an effect on crew operations significantly different from that experienced during the Mercury, Gemini, and Apollo missions. A summary of the opinions and experience of the three Skylab flightcrews in using these Skylab-unique systems is given. The designs that the crews considered completely successful as compared to the preflight expectations and those designs that turned out to be unsuitable and that should be approached differently in future missions are discussed. Differences in crew opinions about the same system are noted where appropriate, and spacecraft lessons learned by the flightcrews are summarized.
    Keywords: SPACE VEHICLES
    Type: AAS PAPER 74-119 , Annual Meeting; Aug 20, 1974 - Aug 22, 1974; Los Angeles, CA
    Format: text
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    NASA TECHNICAL REPORTS
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