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  • Polymer and Materials Science  (4,131)
  • BIOTECHNOLOGY  (595)
  • 550 - Earth sciences
  • AERODYNAMICS
  • 1970-1974  (5,203)
  • 1960-1964
  • 1955-1959
  • 1973  (2,686)
  • 1970  (2,517)
Collection
Keywords
Publisher
Years
  • 1970-1974  (5,203)
  • 1960-1964
  • 1955-1959
Year
  • 1
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    In:  Other Sources
    Publication Date: 2011-12-21
    Description: Modifications for Apollo space flight feeding program
    Keywords: BIOTECHNOLOGY
    Type: AEROSPACE FOOD TECHNOL. 1970; P 5-13
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  • 2
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    In:  CASI
    Publication Date: 2005-11-30
    Description: Impact, emergency escape and crash survival protection are studied. Accleration, the G system of units, data interpretation, and human tolerance limits are summarized, along with physiological and biochemical response to impact. Biomechanical factors of impact are also cited.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 221-295
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  • 3
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Semi-solid, dehydrated, rehydratable, thermally stabilized wet, and intermediate moisture food development for space flights
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON PROC. OF THE 7TH ANN. WORKING GROUP ON EXTRATERREST. RESOURCES 1970; P 39-49
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  • 4
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Compressed dehydrated food for aircraft crews
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 117-119
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  • 5
    Publication Date: 2005-11-27
    Description: Reliability, weight, size, and power supplies as factors in designing microwave ovens for spacecraft
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 175-176
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  • 6
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Research and development of microwave ovens for use in aircraft
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 171-174
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  • 7
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Laboratory and flight performance tests of integral heating units for food preparation
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 177-181
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  • 8
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Projected research and development for selected and alternative subsystems of integrated life support system
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 697-713
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  • 9
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Steam desorbed resin for carbon dioxide removal in spacecraft cabin atmosphere
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 157-205
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  • 10
    Publication Date: 2005-11-27
    Description: Jet induced flow field effects on V/STOL aircraft in subsonic transition flight
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 683-702
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  • 11
    Publication Date: 2005-11-27
    Description: Iterative method for designing supersonic body of revolution from surface pressure distribution
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 75-84
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  • 12
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    In:  CASI
    Publication Date: 2005-11-30
    Description: Human energy is discussed in terms of the whole man. The physical work a man does, the heat he produces, and the quantity of oxygen he takes from the air to combine with food, the fuel source of his energy, are described. The daily energy exchange, work and heat dissipation, oxygen costs of specific activities, anaerobic work, and working in space suits are summarized.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 847-879
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  • 13
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    In:  CASI
    Publication Date: 2005-11-30
    Description: The capabilities and limitations of man as an element in a closed loop control system under normal environmental conditions are described. Controller characteristics are enumerated, using manual control, quasilinear models, pilot opinion and ratings, compensatory tracking, optimum control models, motion cues, multiple input tracking, multiple loop tracking, transmission delays, and adaptive manual control. Various controls, manipulators, and displays are also considered.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 751-806
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  • 14
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    In:  CASI
    Publication Date: 2005-11-30
    Description: Noise and blast environments are described, providing a definition of units and techniques of noise measurement and giving representative booster-launch and spacecraft noise data. The effects of noise on hearing sensitivity and performance are reviewed, and community response to noise exposure is discussed. Physiological, or nonauditory, effects of noise exposure are also treated, as are design criteria and methods for minimizing the noise effects of hearing sensitivity and communications. The low level sound detection and speech reception are included, along with subjective and behavioral responses to noise.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 693-750
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  • 15
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    In:  CASI
    Publication Date: 2005-11-30
    Description: Rotary acceleration is found to be a manifestation of angular acceleration, and is always present during steady state spinning or tumbling, even when the angular velocity is constant. Subjective reactions and tolerances, performance, physiological effects, and pathological effects are reviewed for rotary acceleration. Thresholds for stimulation perception by angular acceleration in man are presented in tabular form.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 191-219
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  • 16
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    In:  CASI
    Publication Date: 2005-11-30
    Description: Properties of elements and compounds are considered which make up or may be added to a gaseous environment suitable for humans. Oxygen and carbon dioxide are emphasized; nitrogen and the noble gases are also cited. Other gaseous compounds, such as carbon monoxide, methane, and sulfur hexafluoride, are briefly mentioned.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 35-63
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  • 17
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    In:  CASI
    Publication Date: 2005-11-30
    Description: The subjective effects of sustained acceleration are discussed, including positive, negative, forward, backward, and lateral acceleration effects. Physiological effects, such as retinal and visual response, unconsciousness and cerebral function, pulmonary response, and renal output, are studied. Human tolerance and performance under sustained acceleration are ascertained.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 149-190
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  • 18
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    In:  CASI
    Publication Date: 2005-11-30
    Description: Tolerance levels, physiological effects, and performance degradation during simultaneous or sequential exposures to two environmental stresses, and also three or more simultaneous stresses are described. Environmental stress combinations are characterized by four descriptors: order of occurrence, duration of exposure, severity of exposure, and type of interaction. Combined stress data and facilities for combined stress study are briefly mentioned.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 881-914
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  • 19
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    In:  CASI
    Publication Date: 2005-11-30
    Description: The problems in human comfort in heat stress are emphasized, with less emphasis placed upon cold exposure problems. Physiological parameters related to human thermal interactions are discussed, as well as data concerning thermal protective clothing. The energy balance equation, heat transfer equation, thermal comfort, heat stress, and cold stress are also considered. A two node model of human temperature regulation in FORTRAN is appended.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 65-148
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  • 20
    Publication Date: 2005-11-27
    Description: Shelf-stable rehydratable and intermediate moisture foods and moisture mimetic products
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 125-129
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  • 21
    Publication Date: 2005-11-27
    Description: Human factors and standardization of food item selection for Manned Orbiting Laboratory feeding system
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 21-29
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  • 22
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Physicochemical synthesis of food for long term space flights
    Keywords: BIOTECHNOLOGY
    Type: AEROSPACE FOOD TECHNOL. 1970; P 133-140
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  • 23
    Publication Date: 2005-11-27
    Description: Logistics of feeding Boeing 707 and 747 aircraft passengers
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 109-111
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  • 24
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Airline and space feeding systems, and work-rest division of astronauts day
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 105-108
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  • 25
    Publication Date: 2005-11-27
    Description: Ground wind loads on reusable space shuttles
    Keywords: AERODYNAMICS
    Type: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 143-160
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  • 26
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Space shuttle buffeting and aerodynamic noise
    Keywords: AERODYNAMICS
    Type: SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 238-247
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  • 27
    Publication Date: 2005-11-27
    Description: Ducted fan interference analysis for transport aircraft
    Keywords: AERODYNAMICS
    Type: NASA, WASHINGTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970; P 703-719
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  • 28
    Publication Date: 2005-11-27
    Description: Time-dependent numerical method for blunt body flow field solutions
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 177-195
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  • 29
    Publication Date: 2005-11-27
    Description: Prediction methods for boundary layer and flow field characteristics in shock wave-boundary layer interaction
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 515-539
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  • 30
    Publication Date: 2005-11-27
    Description: Numerical analysis of three dimensional viscous supersonic flow fields about slender bodies
    Keywords: AERODYNAMICS
    Type: NASA, WASHINTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970; P 265-321
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  • 31
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Possible feeding systems for long term space missions after Apollo Applications Program
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 145-149
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  • 32
    Publication Date: 2005-11-27
    Description: Food system integration into aircraft as joint responsibility of airframe manufacturers and air carriers
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 193-202
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  • 33
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    In:  CASI
    Publication Date: 2005-11-27
    Description: System integration of Boeing 747 lower lobe galley
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 183-191
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  • 34
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    In:  CASI
    Publication Date: 2005-11-27
    Description: High temperature oven with fast-circulated hot air as possible equipment for spacecraft
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 169-170
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  • 35
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Transworld airline feeding operations
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 112-114
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  • 36
    Publication Date: 2005-11-27
    Description: Systems analysis of feeding system for Manned Orbiting Laboratory
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 43-55
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  • 37
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Trace gas control method for decontamination of integrated life support system
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 253-283
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  • 38
    Publication Date: 2005-11-27
    Description: Method of characteristics for computerized design of optimal supersonic inlets
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 569-581
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  • 39
    Publication Date: 2005-11-27
    Description: Aerodynamic method of characteristics for pressure field calculations about wing-body combinations
    Keywords: AERODYNAMICS
    Type: L METHODS IN AIRCRAFT AERODYN. 1970; P 215-227
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  • 40
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Numerical analysis of propeller-wing flow interaction with slipstreams
    Keywords: AERODYNAMICS
    Type: NASA, WASHINGTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970; P 721-742
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  • 41
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Weight and power aspects of integrated life support system having either nitrogen, helium, or neon atmosphere
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 715-738
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  • 42
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Environmental control and life support systems design criteria for prolonged manned space flight mission
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 573-696
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  • 43
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Vacuum decomposition of human waste materials during prolonged space flight in controlled atmosphere
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 425-472
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  • 44
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Oxygen and nitrogen storage requirements for integrated life support system
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 65-108
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  • 45
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    Publication Date: 2005-11-27
    Description: Outline of study on regenerative advanced integrated life support systems
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 9-64
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  • 46
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Water electrolysis system for carbon dioxide reduction and oxygen generation in closed cabin atmosphere
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 117-156
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  • 47
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    In:  CASI
    Publication Date: 2005-11-30
    Description: The penetrating ionizing space radiations are found to be extremely diverse in the energy range of both their particulate and their electromagnetic components. Radiation terms and measures and ionizing radiation classes and sources are presented. Whole body radiation effects are examined, including radiation intensity and rate effectiveness factors. Radiation effects on specific body systems, such as blood, skin, visual, and reproductive systems are also discussed.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 417-454
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  • 48
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    Publication Date: 2005-11-30
    Description: The effects of alterations in barometric pressure on human beings are described. Human tolerances for gaseous environments and low and high barometric pressure are discussed, including effects on specific areas, such as the ear, lungs, teeth, and sinuses. Problems due to trapped gas within the body, high dynamic pressures on the body, and blasts are also considered.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 1-34
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  • 49
    Publication Date: 2005-11-27
    Description: Wind tunnel simulation of ground wind shear and turbulence spectra and application to space shuttle launching
    Keywords: AERODYNAMICS
    Type: NASA. LEWIS RES. CENTER SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 161-175
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  • 50
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    Publication Date: 2005-11-27
    Description: Different techniques of preserving food for military field rations
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 151-163
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  • 51
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    Publication Date: 2005-11-27
    Description: Crude biomasses for nutritional requirements of spacecraft crews
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 141-144
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  • 52
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    Publication Date: 2005-11-27
    Description: Dehydrated and rehydratable meat-type foods for space flight feeding
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 121-123
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  • 53
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    Publication Date: 2005-11-27
    Description: Food selection and preparation plans for Sealab 3
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 79-85
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  • 54
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    Publication Date: 2005-11-27
    Description: Requirements for Apollo Applications Program feeding system
    Keywords: BIOTECHNOLOGY
    Type: AEROSPACE FOOD TECHNOL. 1970; P 57-60
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  • 55
    Publication Date: 2005-11-27
    Description: Advantages and problems of preserving food with ionizing radiation
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 87-100
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  • 56
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    Publication Date: 2005-11-27
    Description: Functional analysis on feeding system for Manned Orbiting Laboratory
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 31-36
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  • 57
    Publication Date: 2005-11-27
    Description: Improved prototype space feeding system for Manned Orbiting Laboratory missions
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 37-41
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  • 58
    Publication Date: 2005-11-27
    Description: Feeding system requirements for Manned Orbiting Laboratory
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 15-19
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  • 59
    Publication Date: 2005-11-27
    Description: Lift and pressure distribution calculations for winged body with leading edge vortices
    Keywords: AERODYNAMICS
    Type: NASA, WASHINGTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970; P 113-129
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  • 60
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    Publication Date: 2005-11-27
    Description: Temperature and humidity control in integrated life support system
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 285-335
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  • 61
    Publication Date: 2005-11-27
    Description: Finite difference solution for compressible turbulent boundary layer equations of swept slab with leading edge blowing
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 417-472
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  • 62
    Publication Date: 2005-11-27
    Description: Review of prediction methods for compressible turbulent boundary layers
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 355-416
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  • 63
    Publication Date: 2005-11-27
    Description: Finite difference analysis of hyperbolic partial differential equations
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 245-264
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  • 64
    Publication Date: 2005-11-27
    Description: Computer programs for predicting flow field properties in supersonic and hypersonic inlets
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 583-595
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  • 65
    Publication Date: 2005-11-27
    Description: Wing-body interference theory for calculating lift slope and stability at hypersonic speed
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 101-111
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  • 66
    Publication Date: 2005-11-27
    Description: Numerical lifting surface theory with spanwise distribution of control points
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 1-35
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  • 67
    Publication Date: 2005-11-27
    Description: Method of characteristics for flow field analysis on elliptical winged body
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 159-176
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  • 68
    Publication Date: 2005-11-27
    Description: Finite element method for predicting aerodynamic characteristics of wing-body combinations
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 37-51
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  • 69
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Solid electrolyte process for carbon dioxide removal and oxygen generation in integrated life support system
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 207-251
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  • 70
    Publication Date: 2005-11-27
    Description: Potential flow solution for VTOL inlets in static and crossflow operation
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 659-681
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  • 71
    Publication Date: 2005-11-27
    Description: Analysis of secondary flow effects in propeller and rotor boundary layers
    Keywords: AERODYNAMICS
    Type: NASA, WASHINGTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970; P 473-514
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  • 72
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Freeze-dried diet and personal hygiene for space crew
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 473-518
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  • 73
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Water reclamation and purification method for integrated life support system
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 337-424
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  • 74
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Atmospheric pressure and composition control system for manned spacecraft cabin atmosphere
    Keywords: BIOTECHNOLOGY
    Type: TRADE-OFF STUDY AND CONCEPTUAL DESIGNS OF REGENERATIVE ADVANCED INTEGRATED LIFE SUPPORT SYSTEMS JAN. 1970; P 109-115
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  • 75
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Finite difference method for transonic flow solution in axial stator
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 597-621
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  • 76
    Publication Date: 2005-11-27
    Description: Method of characteristics for calculating oblique shock wave interaction with turbulent boundary layer
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 541-567
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  • 77
    Publication Date: 2005-11-27
    Description: Aerodynamic forces in supersonic panel flutter
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 335-353
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  • 78
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    In:  CASI
    Publication Date: 2005-11-27
    Description: Static laminar Coanda jet flow around circular cylinder with external flow entrainment
    Keywords: AERODYNAMICS
    Type: NASA, WASHINGTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970; P 197-214
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  • 79
    Publication Date: 2005-11-27
    Description: Correlation method for estimating pressure distribution over elliptic supersonic cones
    Keywords: AERODYNAMICS
    Type: L. METHODS IN AIRCRAFT AERODYN. 1970; P 85-99
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  • 80
    Publication Date: 2005-11-27
    Description: Calculation methods for predicting transonic aerodynamic characteristics of wing-body combinations
    Keywords: AERODYNAMICS
    Type: NASA, WASHINGTON ANAL. METHODS IN AIRCRAFT AERODYN. 1970; P 53-73
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  • 81
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    In:  CASI
    Publication Date: 2009-11-16
    Description: Man's reactions to vibration are emphasized rather than his reactions to the vibrational characteristics of vehicles. Vibrational effects studies include: performance effects reflected in tracking proficiency, reaction time, visual impairment, and other measures related to man's ability to control a system; physiological reactions; biodynamic responses; subjective reactions; and human tolerance limits. Technological refinements in shaker systems and improved experimental designs are used to validate the data.
    Keywords: BIOTECHNOLOGY
    Type: BioTechnol., Inc. Bioastronaut. Data Book, 2d Ed.; p 297-348
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  • 82
    Publication Date: 2009-11-17
    Description: Operational procedures for food service in nuclear submarines
    Keywords: BIOTECHNOLOGY
    Type: NASA, WASHINGTON AEROSPACE FOOD TECHNOL. 1970; P 63
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  • 83
    Publication Date: 2009-11-17
    Description: Prediction of steady and unsteady airloads on space shuttles
    Keywords: AERODYNAMICS
    Type: NASA. LEWIS RES. CENTER SPACE TRANSPORTATION SYSTEM TECHNOL. SYMP., VOL. 2 JUL. 1970; P 223-237
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  • 84
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    In:  CASI
    Publication Date: 2006-01-11
    Description: A rotating space station simulator is being used to obtain data on man's performance in a rotating environment. At present the facility is being used to assess the effects of rotation on man's walking capabilities on circular and flat walls at g-levels from 0.05 to 0.75g. Some of the preliminary results are reviewed.
    Keywords: BIOTECHNOLOGY
    Type: Fifth Symp. on the Role of the Vestibular Organs in Space Exploration; p 67-72
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  • 85
    Publication Date: 2006-01-11
    Description: Three groups of 10 subjects each were exposed to stepwise increments of cross coupled angular accelerations in three visual modes: internal visual reference (IVR), external visual reference (EVR), and vision absent (VA). The subjects in the IVR condition required significantly greater amounts of stimulus exposure to neutralize their illusory subjective reactions. They also suffered a greater loss of well-being and a more marked incidence of motion sickness than did subjects in the EVR and VA conditions. The same 30 subjects were reexposed to the same graded cross coupled stimulation 1 week later. This time, however, all the subjects were tested under only the IVR condition. All three groups showed some positive transfer of adaptation, but only the IVR-IVR combination required significantly fewer head motions to achieve the same level of adaptation on the second occasion. Taken overall, however, the most efficient and least disturbing route to adaptation at the completion of the second test was via the VA-IVR combination.
    Keywords: BIOTECHNOLOGY
    Type: NASA, Washington Fifth Symp. on the Role of the Vestibular Organs in Space Exploration; p 87-97
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  • 86
    Publication Date: 2006-01-11
    Description: The effects of increasing artificial gravity exposure on four aspects of physiological fitness are examined in four young men who, prior to exposure, were deconditioned with bed rest and water immersion. The four aspects of physiological fitness are orthostatic tolerance, exercise tolerance, forearm endurance, and maximum strength. Orthostatic tolerance was sharply reduced by deconditioning and was substantially improved by walking in simulated lunar gravity (1/6 g) for 2.5 hours daily for 7 days or by walking in 1/2 g and 1 g for 1 hour daily for 3 days. Exercise tolerance was also sharply reduced by deconditioning but did not significantly improve with increasing g-exposure. Walking in 1 g for 1 hour daily for 3 days raised exercise tolerance only a little above the low produced by deconditioning. Forearm endurance and maximum strength were relatively unaffected by deconditioning and subsequent g-exposure.
    Keywords: BIOTECHNOLOGY
    Type: NASA, Washington Fifth Symp. on the Role of the Vestibular Organs in Space Exploration; p 73-83
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  • 87
    Publication Date: 2006-01-11
    Description: A ground based research program is now being undertaken to provide data concerning the effects of a rotating environment on man's ability to adequately perform gross and fine psychomotor tasks. Emphasis is being placed on establishing the levels of artificial gravity and rates and radii of rotation required in future space systems for preservation of crew performance and comfort. An experimental study utilizing a rotational facility to investigate crew mobility, cargo transfer and handling, and fine motor coordination at radii up to 24 meters and at rotational rates up to 5 rpm is reported.
    Keywords: BIOTECHNOLOGY
    Type: Fifth Symp. on the Role of the Vestibular Organs in Space Exploration; p 55-65
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  • 88
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    In:  CASI
    Publication Date: 2006-01-11
    Description: The unique characteristics of artificial gravity that affect human performance and physiology in an artificial gravity environment are reviewed. The rate at which these unique characteristics change decreases very rapidly with increasing radius of a rotating vehicle used to produce artificial gravity. Reducing their influence on human performance or physiology by increasing radius becomes a situation of very rapidly diminishing returns. A review of several elements of human performance has developed criteria relative to the sundry characteristics of artificial gravity. A compilation of these criteria indicates that the maximum acceptable rate of rotation, leg heaviness while walking, and material handling are the factors that define the minimum acceptable radius. The ratio of Coriolis force to artificial weight may also be significant. Based on current knowledge and assumptions for the various criteria, a minimum radius between 15.2 and 16.8 m seems desirable.
    Keywords: BIOTECHNOLOGY
    Type: Fifth Symp. on the Role of the Vestibular Organs in Space Exploration; p 23-33
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  • 89
    Publication Date: 2004-12-03
    Keywords: AERODYNAMICS
    Type: its Supercritical Wing Technol.: A Report on Flight Evaluation; p 59-70
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  • 90
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    Publication Date: 2006-01-11
    Description: A 56-day chamber simulation of Skylab was successfully completed. The atmosphere (5 psi, 70 percent oxygen, 30 percent nitrogen, 5 mm carbon dioxide) and medical features including a 21-day pre- and 18-day post-test medical protocols were closely simulated. No apparent crew health problems were induced by the atmosphere, semiclosed environment, or other test features; and no appreciable crew degradation appeared over this period. The chamber and associated systems performed without major problems.
    Keywords: BIOTECHNOLOGY
    Type: Skylab Med. Expt. Altitude Test (SMEAT); 46 p
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  • 91
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    Publication Date: 2006-01-11
    Description: The brief history of the Skylab altitude test crewmen is followed by an outline of their training in conducting medical experiments, emergency medical procedures, communications, and housekeeping practices during prolonged exposure to the Skylab simulation environment.
    Keywords: BIOTECHNOLOGY
    Type: Skylab Med. Expt. Altitude Test (SMEAT); 7 p
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  • 92
    Publication Date: 2006-01-11
    Description: Biomedical support hardware for SMEAT consisted basically of two systems, the inflight medical support system, and the operational bioinstrumentation system. The former is essentially a diagnostic and therapeutic kit; the latter is a belt equipped with sensors worn by the crewman to permit monitoring of his vital signs. Special attention was given during to the use and verification of the items in the systems so that changes required in the equipment could be pinpointed and effected prior to the Skylab mission. During the in-chamber testing, evaluations were made of the effectiveness of the proposed microbiology procedures, techniques, equipment, and the stability of media and reagents over the extended period of storage.
    Keywords: BIOTECHNOLOGY
    Type: Skylab Med. Expt. Altitude Test (SMEAT); 8 p
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  • 93
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    Publication Date: 2006-01-11
    Description: Skylab experiment M487, habitability crew quarters, is designed to provide an operational evaluation of the Skylab habitat by gathering data regarding the manner in which crewmen carry out their daily living and working routines during the missions. The success of the Skylab habitability experiment depends, in large measure, on the adequacy of the data collection instruments and the manner in which they are used.
    Keywords: BIOTECHNOLOGY
    Type: Skylab Med. Expt. Altitude Test (SMEAT); 11 p
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  • 94
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    In:  CASI
    Publication Date: 2006-01-11
    Description: The Skylab specimen mass measurement device was operated throughout the altitude test in close simulation of the 56-day Skylab mission. It performed operational specimen measurements well until it was passed out of the chamber for replacement of the specimen hold-down and was autoclaved prior to return. Fecal measurements were typically made with less than one percent error.
    Keywords: BIOTECHNOLOGY
    Type: Skylab Med. Expt. Altitude Test (SMEAT); 16 p
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  • 95
    Publication Date: 2006-01-11
    Description: Astronaut work performance during the preparation and execution of experiments in simulated Skylab tests was analyzed according to time and motion in order to evaluate the efficiency and consistency of performance (adaptation function) for several different types of activity over the course of the mission; to evaluate the procedures to be used by the same experiment in Skylab; to generate characteristic adaptation functions for later comparison with Skylab data; and to examine astronaut performance for any behavioral stress due to the environment. The overall results indicate that the anticipated adaptation function was obtained both for individual and for averaged data.
    Keywords: BIOTECHNOLOGY
    Type: NASA. Johnson Space Center Skylab Med. Expt. Altitude Test (SMEAT); 7 p
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  • 96
    Publication Date: 2006-03-28
    Description: The dynamic characteristics of a man were investigated by the resonance method, by means of recordings of the amplitude-frequency characteristics of a vibrator straight arm human body system on a standard automatic recorder. Experiments were carried out with a specially constructed vibrator, the moving system of which was fastened to a bronze suspension with small losses. Vibrations of the handle, fastened to the moving system, were recorded with an accelerometer. The mass of the moving system m, rigidity of the suspension k and friction coefficient r of the vibrator (calibration) were determined by exact formulas.
    Keywords: BIOTECHNOLOGY
    Type: Cybernetic Diagnostics of Mech. Systems with Vibro-acoustic Phenomena (NASA-TT-F-14899); p 83-86
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  • 97
    Publication Date: 2006-03-27
    Description: Some of the principal results obtained in three series of measurements of fluctuating surface pressures induced on externally blown flaps by jet impingment are presented. Large- and small-scale models and hot- and cold-flow tests are considered. The discussion sets forth scaling parameters and consistent features of the root-mean-square values and spectra of the loading. Implications of these results with regard to sonic fatigue are indicated.
    Keywords: AERODYNAMICS
    Type: STOL Technol.; p 131-142
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  • 98
    Publication Date: 2011-10-14
    Description: In-flight studies of the overall and local components of drag of many types of aircraft were conducted. The primary goal of these studies was to evaluate wind-tunnel and semiempirical prediction methods. Some evaluations are presented in this paper which may be summarized by the following observations: Wind-tunnel predictions of overall vehicle drag can be accurately extrapolated to flight Reynolds numbers, provided that the base drag is removed and the boattail areas on the vehicle are small. The addition of ablated roughness to lifting body configurations causes larger losses in performance and stability than would be expected from the added friction drag due to the roughness. Successful measurements of skin friction have been made in flight to Mach numbers above 4. A reliable inflatable deceleration device was demonstrated in flight which effectively stabilizes and decelerates a lifting aircraft at supersonic speeds.
    Keywords: AERODYNAMICS
    Type: AGARD Aerodyn. Drag; 12 p
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  • 99
    Publication Date: 2011-10-14
    Description: The basic unsteady aerodynamic environment of the rotary wing is summarized. Some of the observed trends in the state of the art are discussed. Some of the research needs that will require attention are reported. A review of a number of research investigations as a part of a joint NASA/Army rotorcraft project is presented. The research is directed toward achieving a better understanding of rotor unsteady airfoils. The investigations include: (1) rotor maneuver loads; (2) level flight and maneuver wake prediction; (3) tip-vortex flow; (4) blade-vortex interactions; (5) dynamic stall; (6) transient Mach number air loads; and (7) development of variable geometry rotors.
    Keywords: AERODYNAMICS
    Type: AGARD Aerodyn. of Rotary Wings; 20 p
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  • 100
    Publication Date: 2011-08-16
    Description: Primate restraint harness of nylon jacket and cotton cot on aluminum frame padded seat for bone resorption and calcium metabolism studies
    Keywords: BIOTECHNOLOGY
    Type: ; YAL SOCIETY (
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