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  • SPACE SCIENCES  (858)
  • SPACE VEHICLES  (327)
  • 1970-1974  (1,185)
  • 1974  (1,185)
  • 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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    Appendices for the Space Applications program, 1974 (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: To achieve truly low cost system design with direct evolution for inorbit shuttle resupply, a modular building block approach has been adopted. The heart of the modular building block concept lies in the ability to use a common set of nonoptimized subsystems in such a way that a wide variety of missions can be flown with no detrimental impact on performance. By standardizing the mechanical configurations and electrical interfaces of the subsystem modules, and by designing each of them to be structurally and thermally independent entities, it is possible to cluster these building blocks or modules about an instrument system so as to adequately perform the mission without the need for subsystem redevelopments for each mission. This system concept offers the following capabilities: (1) the ability to launch and orbit the observatory by either the Delta, the Titan, or the space shuttle. (2) the ability to completely reconfigure the spacecraft subsystems for different launch vehicles, and (3) the ability to perform in-orbit resupply and/or emergency retrieval of the observatory.
    Keywords: SPACE SCIENCES
    Type: NASA-TM-X-70205
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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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
  • 4
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    Quasars, pulsars, black holes and HEAO's (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-28
    Description: Astronomical surveys are discussed by large X-ray, gamma ray, and cosmic ray instruments carried onboard high-energy astronomy observatories. Quasars, pulsars, black holes, and the ultimate benefits of the new astronomy are briefly discussed.
    Keywords: SPACE SCIENCES
    Type: NASA-EP-120
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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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
  • 6
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    The geologic setting of Boulder 1, Station 2 (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-08-27
    Description: Apollo 17 landed on the flat floor of a deep, narrow valley embayed in the mountainous highlands that comprise the southeastern rim of Mare Serenitatis. Serenitatis is one of the youngest multiringed basins on the lunar nearside and is underlain by a mascon. The valley of Taurus-Littrow, which is radial to the basin, is generally interpreted as a graben formed as a result of structural adjustments of the lunar crust in response to the Serenitatis event.
    Keywords: SPACE SCIENCES
    Type: Smithsonian Astrophys. Obs. Interdisciplinary Studies of Samples From Boulder 1, Sta. 2, Apollo 17, Vol. 1; p 1-8
    Format: text
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    NASA TECHNICAL REPORTS
  • 7
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    Skylab mission report, third visit (1974)
    In:  CASI
    Details
    Publication Date: 2019-08-14
    Description: An evaluation is presented of the operational and engineering aspects of the third Skylab visit, including information on the performance of the command and service module and the experiment hardware, the crew's evaluation of the visit, and other visit-related areas of interest such as biomedical observations. The specific areas discussed are contained in the following: (1) solar physics and astrophysics investigations; (2) Comet Kohoutek experiments; (3) medical experiments; (4) earth observations, including data for the multispectral photographic facility, the earth terrain camera, and the microwave radiometer/scattermometer and altimeter; (5) engineering and technology experiments; (6) food and medical operational equipment; (7) hardware and experiment anomalies; and (8) mission support, mission objectives, flight planning, and launch phase summary. Conclusions discussed as a result of the third visit to Skylab involve the advancement of the sciences, practical applications, the durability of man and systems in space, and spaceflight effectiveness and economy.
    Keywords: SPACE SCIENCES
    Type: NASA-TM-X-70385 , JSC-08963
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 8
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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
  • 9
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    Preliminary results on the atmospheres of Io and Jupiter from the Pioneer 10 S-band occultation experiment (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-08-13
    Description: The preliminary analysis of data from the Pioneer 10 S-band radio occultation experiment has revealed the presence of an ionosphere on the Jovian satellite Io having an electron density peak of about 60,000 electrons per cubic centimeter at an altitude of approximately 60 to 140 kilometers. This suggests the presence of an atmosphere having a surface number density of about 10 billion to one trillion per cubic centimeter, corresponding to an atmospheric surface pressure of between .1 and 10 nanobar, at or below the detection threshold of the Beta Scorpii stellar occultation. A measurement of the atmosphere of Jupiter was obtained down to the level of about 80 millibars, indicating a large temperature increase at about the 20 millibar level, which cannot be explained by the absorption of solar radiation by methane alone and can possibly be due to absorption by particulate matter.
    Keywords: SPACE SCIENCES
    Type: Science; 183; Jan. 25
    Format: text
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    NASA TECHNICAL REPORTS
  • 10
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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
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