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  • 1
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    Convective heat transfer to a blunt lifting body (1960)
    In:  CASI
    Details
    Publication Date: 2004-12-03
    Keywords: GENERAL
    Type: Joint Conf. on Lifting Manned Hypervelocity and Reentry Vehicles, part 1; p 121-140
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    Preliminary studies of manned satellites. Wingless configurations - Lifting body (1958)
    In:  CASI
    Details
    Publication Date: 2005-01-20
    Keywords: unknown
    Type: NACA CONF. ON HIGH-SPEED AERODYN. 1958; P 35-44
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    HEAT TRANSFER TO BLUNT AXIALLY SYMMETRIC BODIES (1960)
    In:  CASI
    Details
    Publication Date: 2019-05-11
    Description: Comparison of heat transfer rates to blunt bodies of revolution & evaluation of effects of body-nose geometry on heat transfer rates
    Keywords: AIRCRAFT
    Type: NASA-TM-X-391
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 4
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    Study of airborne science experiment management concepts for application to space shuttle. Volume 1: Executive summary (1973)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The management concepts and operating procedures are documented as they apply to the planning of shuttle spacelab operations. Areas discussed include: airborne missions; formulation of missions; management procedures; experimenter involvement; experiment development and performance; data handling; safety procedures; and applications to shuttle spacelab planning. Characteristics of the airborne science experience are listed, and references and figures are included.
    Keywords: SPACE SCIENCES
    Type: NASA-TM-X-62288
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    Shuttle sortie simulation using a Lear jet aircraft: Mission no. 1 (assess program) (1972)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The shuttle sortie simulation mission of the Airborne Science/Shuttle Experiments System Simulation Program which was conducted using the CV-990 aircraft is reported. The seven flight, five day mission obtained data on experiment preparation, type of experiment components, operation and maintenance, data acquisition, crew functions, timelines and interfaces, use of support equipment and spare parts, power consumption, work cycles, influence of constraints, and schedule impacts. This report describes the experiment, the facilities, the operation, and the results analyzed from the standpoint of their possible use in aiding the planning for experiments in the Shuttle Sortie Laboratory.
    Keywords: SPACE SCIENCES
    Type: NASA-TM-X-62283
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 6
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    Design and performance of the Ames electric-arc shock tunnel (1973)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: A high enthalpy shock tunnel using arc-heated helium as the driver gas was designed for gas dynamic research at total stream energies from 7,000 to 35,000 j/g. The arc driver was found to be a relatively efficient energy converter. Tailored shock Mach numbers from 11.5 to 14.6 in air were demonstrated. A nozzle calibration with a total stream enthalpy of 18,600 j/g of air gave test times of 1.5 to 2.0 m sec at flow Mach numbers from 16 to 24.
    Keywords: FACILITIES, RESEARCH, AND SUPPORT
    Type: NASA-TM-X-2814 , A-4606
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 7
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    Shuttle spacelab simulation using a Lear jet aircraft: Mission no. 3 (ASSESS program) (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The third ASSESS mission using a Lear Jet aircraft conducted to continue the study of scientific experiment operations in a simulated Spacelab environment. Prior to the mission, research planning and equipment preparation were observed and documented. A flight readiness review for the experiment was conducted. Nine of the ten scheduled flights were completed during simulation mission and all major science objectives were accomplished. The equipment was well qualified for flight and gave little trouble; telescope malfunctions occurred early in the mission and were corrected. Both real-time and post-observation data evaluation were used to assess research progress and to plan subsequent flight observations for maximum effectiveness.
    Keywords: RESEARCH AND SUPPORT FACILITIES (AIR)
    Type: NASA-TM-X-62410 , A-5907
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 8
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    Analysis of the flow in a 1-MJ electric-arc shock tunnel (1972)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: In the electric-arc-heated shock tunnel, the facility performance over a range of shock Mach numbers from 7 to 19 was evaluated. The efficiency of the arc-heated driver is deduced using an improved form of the shock tube equation. A theoretical and experimental analysis is made of the tailored-interface condition. The free stream properties in the test section, with nitrogen as the test gas, are evaluated using a method based on stagnation point, heat transfer measurements.
    Keywords: FACILITIES, RESEARCH, AND SUPPORT
    Type: NASA-TN-D-6865 , A-4341
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 9
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    NASA/ESA CV-990 spacelab simulation (1976)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: Simplified techniques were applied to conduct an extensive spacelab simulation using the airborne laboratory. The scientific payload was selected to perform studies in upper atmospheric physics and infrared astronomy. The mission was successful and provided extensive data relevant to spacelab objectives on overall management of a complex international payload; experiment preparation, testing, and integration; training for proxy operation in space; data handling; multiexperimenter use of common experimenter facilities (telescopes); multiexperiment operation by experiment operators; selection criteria for spacelab experiment operators; and schedule requirements to prepare for such a spacelab mission.
    Keywords: LAUNCH VEHICLES AND SPACE VEHICLES
    Type: NASA-TM-X-73105 , ESA-SL-75-2 , A-6442
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 10
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    Spacelab simulation using a Lear Jet aircraft: Mission no. 4 (ASSESS program) (1975)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The fourth ASSESS Spacelab simulation mission utilizing a Lear Jet aircraft featured trained experiment operators (EOs) in place of the participating scientists, to simulate the role and functions of payload specialists in Spacelab who may conduct experiments developed by other scientists. The experiment was a broadband infrared photometer coupled to a 30-cm, open port, IR telescope. No compromises in equipment design or target selection were made to simplify operator tasks; the science goals of the mission were selected to advance the mainline research program of the principle investigator (PI). Training of the EOs was the responsibility of the PI team and consisted of laboratory sessions, on-site training during experiment integration, and integrated mission training using the aircraft as a high-fidelity simulator. The EO permission experience in these several disciplines proved adequate for normal experiment operations, but marginal for the identification and remedy of equipment malfunctions. During the mission, the PI utilized a TV communication system to assist the EOs to overcome equipment difficulties; both science and operations were successfully implemented.
    Keywords: GROUND SUPPORT SYSTEMS AND FACILITIES (SPACE)
    Type: NASA-TM-X-62474 , A-6245
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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