NASA SPACE VEHICLE DESIGN CRITERIA PAPERS
NASA/SP-8001-REV, Cole Jr.*, H.A. and Erickson*, A.L. and Rainey**, A.G., Buffeting during atmospheric ascent, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *Ames Research, **Langley Research Center, May, 1964, pp. 19, Format(s): PDF 1437k
NASA/SP-8002, Flight-loads measurements during launch and exit, NASA (Washington, DC, United States), December, 1964, pp. 8, Format(s): PDF 649k
NASA/SP-8003, Flutter, buzz, and divergence, NASA (Washington, DC, United States), July, 1964, pp. 10, Format(s): PDF 941k
NASA/SP-8004, Dowell*, E.H., Panel flutter, NASA SPACE VEHICLE DESIGN CRITERIA (STRUCTURES), NASA (Washington, DC, United States), *Princeton University, Langley Research Center, June, 1972, pp. 51, Format(s): PDF 4933k
NASA/SP-8005-REV, Solar
electromagnetic radiation, NASA SPACE VEHICLE DESIGN CRITERIA (Environment),
NASA (Washington, DC, United States), May, 1971, pp. 34, Format(s): PDF 3324k
Values
for solar constant and solar spectral irradiance based on air and spaceborne
observations for use in design of spacecraft, space vehicles, subsystems, and
experiments
NASA/SP-8006, Local Steady Aerodynamic Loads During Launch and Exit, NASA (Washington, DC, United States), May, 1965, pp. 12, Format(s): PDF 1884k
NASA/SP-8007, Seide*, P. and Weingarten*, V. I. and Peterson**, J.P., Buckling of thin-walled circular cylinders, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *University of Southern California, **NASA Langley Research Center., September, 1965, pp. 56, Format(s): PDF 4550k
NASA/SP-8008, Prelaunch ground wind loads, NASA (Washington, DC, United States), November, 1965, pp. 16, Format(s): PDF 2298k
NASA/SP-8009, Propellant slosh loads, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), August, 1968, pp. 30, Format(s): PDF 2591k
NASA/SP-8010, Models of Mars' atmosphere (1974), NASA SPACE VEHICLE DESIGN CRITERIA (Environment), NASA (Washington, DC, United States), NASA Goddard Space Flight Center, December, 1974, pp. 53, Format(s): PDF 5284k
NASA/SP-8011, Models of Venus atmosphere (1972), NASA SPACE VEHICLE DESIGN CRITERIA (ENVIRONMENT), NASA (Washington, DC, United States), NASA Goddard Space Flight Center (Greenbelt, MD, United States), September, 1972, pp. 63, Format(s): PDF 3615k
NASA/SP-8012, Archer, J.S., Natural vibration modal analysis, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), NASA Langley Research Center., September, 1968, pp. 34, Format(s): PDF 2059k
NASA/SP-8013, Cour-Palais, B.G., Meteoroid environment model - 1969 [near earth to lunar surface], NASA SPACE VEHICLE DESIGN CRITERIA (Environment), NASA (Washington, DC, United States), March, 1969, pp. 35, Format(s): PDF 2294k
NASA/SP-8014, Sherman*, M.M., Entry thermal protection, NASA (Washington, DC, United States), NASA Langley Research Center (Hampton, VA, United States), *Philco-Ford Corporation, August, 1968, pp. 37, Format(s): PDF 2252k
NASA/SP-8015, Guidance and navigation for entry vehicles, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control), NASA (Washington, DC, United States), NASA Langley Research Center (Hampton, VA, United States), November, 1968, pp. 47, Format(s): PDF 3155k
NASA/SP-8016, Effects
of structural flexibility on spacecraft control systems, NASA SPACE VEHICLE
DESIGN CRITERIA (Guidance and Control), NASA (Washington, DC, United
States), April, 1969, pp. 47, Format(s): PDF 2829k
Design
and test criteria regarding structural flexibility effects on spacecraft
stability and control systems.
NASA/SP-8017, Harris, M.
and Lyle, R., Magnetic fields - Earth and terrestrial, NASA SPACE VEHICLE
DESIGN CRITERIA (Environment), NASA (Washington, DC, United States), NASA
Goddard Space Flight Center (Greenbelt, MD, United States), March, 1969, pp.
70, Format(s): PDF 4088k
Strength and
direction data on earth and extraterrestrial magnetic fields for guidance in
vehicle design.
NASA/SP-8018, Spacecraft
magnetic torques, NASA SPACE VEHICLE DESIGN CRITERIA (Environment), NASA
(Washington, DC, United States), NASA Electronics Research Center (Cambridge,
MA, United States), March, 1969, pp. 55, Format(s): PDF 2847k
Magnetic torque
resulting from interaction between magnetic properties of spacecraft and
ambient magnetic field
NASA/SP-8019,
Weingarten*, V.I. and Seide*, P., Buckling of thin-walled truncated cones,
NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC,
United States), NASA Langley Research Center and *University of Southern
California, September, 1968, pp. 32, Format(s): PDF 1324k
NASA/SP-8020, Surface Models of Mars (1975), September, 1975, Format(s): PDF 3459k
Data derived
from Mariners 6, 7, and 9, Russian Mars probes, and photographic and radar
observations.
NASA/SP-8021, Models
of earth's atmosphere (90 to 2500 km), NASA SPACE VEHICLE DESIGN CRITERIA
(Environment), NASA (Washington, DC, United States), NASA Goddard Space Flight
Center (Greenbelt, MD, United States), March, 1973, pp. 63, Format(s): PDF
3787k
This monograph
replaces a monograph on the upper atmosphere which was a computerized version
of Jacchia's model. The current model has a range from 90 to 2500 km. In addition
to the computerized model, a quick-look predictio method is given that may be
used to estimate the density for any time and spatial location without using a
computer.
NASA/SP-8022, Goldman*,
R.L., Staging loads - Space vehicle design criteria, NASA SPACE VEHICLE
DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), NASA
Langley Research Center and *Research Institute for Advanced Studies, February,
1969, pp. 30, Format(s): PDF 1493k
Analysis of
loads produced on spacecraft by staging operations and practices to insure that
staging loads are included in spacecraft design.
NASA/SP-8023, Lunar
surface models NASA space vehicle design criteria /Environment/, NASA SPACE
VEHICLE DESIGN CRITERIA (Environment), NASA (Washington, DC, United
States), NASA Marshall Space Flight Center (Huntsville, AL, United States),
May, 1969, pp. 60, Format(s): PDF 2726k
Engineering
models of lunar topography including dielectric, optical, terrain, and crater
models.
NASA/SP-8024, Spacecraft
gravitational torques, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and
Control), NASA (Washington, DC, United States), NASA Marshall Space Flight
Center (Huntsville, AL, United States), May, 1969, pp. 51, Format(s): PDF 2401k
Gravitational
torque effects and analysis for satellite design.
NASA/SP-8025, Solid rocket motor metal cases, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsion), NASA (Washington, DC, United States), April, 1970, pp. 103, Format(s): PDF 6664k
NASA/SP-8026, Spacecraft star trackers, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control), NASA (Washington, DC, United States), Kollsman Instrument Corp. (Elmhurst, NY, United States), July, 1970, pp. 69, Format(s): PDF 3670k
NASA/SP-8027, Spacecraft Radiation Torques, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control), NASA (Washington, DC, United States), October, 1969, pp. 41, Format(s): PDF 2307k
NASA/SP-8028, Entry Vehicle Control, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control), NASA (Washington, DC, United States), NASA Electronics Research Center (Cambridge, MA, United States), November, 1969, pp. 51, Format(s): PDF 2390k
NASA/SP-8029, Aerodynamic And Rocket-Exhaust Heating During Launch And Ascent, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), NASA Langley Research Center (Hampton, VA, United States), May, 1969, pp. 33, Format(s): PDF 2173k
NASA/SP-8030, Transient
Loads From Thrust Excitation, NASA SPACE VEHICLE DESIGN CRITERIA (Structures),
NASA (Washington, DC, United States), NASA Langley Research Center (Hampton,
VA, United States), February, 1969, pp. 28, Format(s): PDF 1320k
Analysis of
transient loads produced by ignition of rocket engine during launch and flight
operations for solid and liquid propellant rocket engines.
NASA/SP-8031, Slosh Suppression NASA Space Vehicle Design Criteria, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), May, 1969, pp. 36, Format(s): PDF 2123k
NASA/SP-8032, Buckling Of Thin-Walled Doubly Curved Shells, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), August, 1969, pp. 36, Format(s): PDF 1535k
NASA/SP-8033, Spacecraft Earth Horizon Sensors, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control), NASA (Washington, DC, United States), December, 1969, pp. 49, Format(s): PDF 2682k
NASA/SP-8034, Spacecraft
Mass Expulsion Torques, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and
Control), NASA (Washington, DC, United States), NASA Langley Research
Center (Hampton, VA, United States), December, 1969, pp. 39, Format(s): PDF
2063k
Spacecraft design considerations associated with disturbance torques caused by mass expulsion.
NASA/SP-8035, Wind
Loads During Ascent, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA
(Washington, DC, United States), June, 1970, pp. 36, Format(s): PDF 2122k
Determining
wind induced structural loads on space vehicle during ascent.
NASA/SP-8036, Effects Of Structural Flexibility On Launch Vehicle Control Systems, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control), NASA (Washington, DC, United States), Massachusetts Inst. of Tech. (Cambridge, MA, United States), February, 1970, pp. 51, Format(s): PDF 2953k
NASA/SP-8037, Assessment and Control of Spacecraft Magnetic Fields, NASA SPACE VEHICLE DESIGN CRITERIA (Environment), NASA (Washington, DC, United States), September, 1970, pp. 30, Format(s): PDF 1699k
NASA/SP-8038, Meteoroid Environment Model, 1970 - Interplanetary and Planetary, NASA SPACE VEHICLE DESIGN CRITERIA (Environment), NASA (Washington, DC, United States), NASA Lyndon B. Johnson Space Center (Houston, TX, United States), October, 1970, pp. 69, Format(s): PDF 3858k
NASA/SP-8039, Solid
Rocket Motor Performance Analysis and Prediction, NASA SPACE VEHICLE DESIGN
CRITERIA (Chemical Propulsion), NASA (Washington, DC, United States), May,
1971, pp. 113, Format(s): PDF 6465k
Current design
practices are reviewed and assessed, and guidance is established for achieving
greater consistency in design, reliability in the end product, and efficiency
in the design effort. The total problem is discussed, and design elements
involved in successful design are identified. Design criteria are described,
and the rule, guide, limitation, or standard which must be imposed on each
essential design element is given. Recommended practices are presented for
satisfying each of the criteria.
NASA/SP-8040, Tiffany*, C.F., Fracture Control of Metallic Pressure Vessels, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *Boeing Co. (Seattle, WA, United States), May, 1970, pp. 65, Format(s): PDF 4610k
NASA/SP-8041, Captive-fired testing of solid rocket motors , NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsion), NASA (Washington, DC, United States), NASA Lewis Research Center (Cleveland, OH, United States), March, 1971, pp. 101, Format(s): PDF 8064k
NASA/SP-8042, Meteoroid Damage Assessment, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), May, 1970, pp. 50, Format(s): PDF 2835k
NASA/SP-8043, Design-Development Testing, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), May, 1970, pp. 35, Format(s): PDF 2000k
NASA/SP-8044, Qualification Testing, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States),NASA Langley Research Center (Hampton, VA, United States), May, 1970, pp. 30, Format(s): PDF 1631k
NASA/SP-8045, Acceptance Testing, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States),NASA Langley Research Center (Hampton, VA, United States), April, 1970, pp. 34, Format(s): PDF 1688k
NASA/SP-8046, Jones*, R. H., Landing Impact Attenuation For Non-Surface-Planing Landers, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *Hughes Aircraft Co. (Culver City, CA, United States), April, 1970, pp. 47, Format(s): PDF 2502k
NASA/SP-8047, Spacecraft Sun Sensors, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), June, 1970, pp. 42, Format(s): PDF 2495k
NASA/SP-8048, Liquid Rocket Engine Turbopump Bearings , NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsion), NASA (Washington, DC, United States), NASA Lewis Research Center (Cleveland, OH, United States), March, 1971, pp. 85, Format(s): PDF 4281k
NASA/SP-8049, The Earth's Ionosphere, NASA SPACE VEHICLE DESIGN CRITERIA (Environment), NASA (Washington, DC, United States), Exotech, Inc. (Washington, DC, United States), March, 1971, pp. 49, Format(s): PDF 2290k
NASA/SP-8050, Archer*,
J. S., Structural Vibration Prediction, NASA SPACE VEHICLE DESIGN CRITERIA
(Structures), NASA (Washington, DC, United States), *TRW Systems Group/TRW
Inc., June, 1970, pp. 41, Format(s): PDF 2473k
Internal loads and stresses caused by space vehicle vibration resulting from induced or natural environments.
NASA/SP-8051, Solid Rocket Motor Igniters, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsion), NASA (Washington, DC, United States), NASA Lewis Research Center (Cleveland, OH, United States), June, 1970, pp. 111,
NASA/SP-8052, Liquid Rocket Engine Turbopump Inducers, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical Propulsion), NASA (Washington, DC, United States), NASA Lewis Research Center (Cleveland, OH, United States), May, 1971, pp. 107, Format(s): PDF 5966k
NASA/SP-8053, Shulman*, H. and Ginell**, W.S, Nuclear and Space Radiation Effects on Materials, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *Teledyne Isotopes, ** McDonnell Douglas Corporation, June, 1970, pp. 48, Format(s): PDF 2519k
NASA/SP-8054, Langley*,
R.W., Space Radiation Protection, NASA SPACE VEHICLE DESIGN CRITERIA
(Structures), NASA (Washington, DC, United States), *McDonnell Douglas
Corporation, June, 1970, pp. 50, Format(s): PDF 3021k
Criteria and
procedures for determining dosage of penetrating space radiation and design.
NASA/SP-8055, Rubin*, S, Prevention of Coupled Structure-Propulsion Instability (POGO), NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *The Aerospace Corporation, October, 1970, pp. 51, Format(s): PDF 3160k
NASA/SP-8056, Mitchell*, D.H., Flight separation mechanisms, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *TRW Systems Group/TRW Inc., October, 1970, pp. 39, Format(s): PDF 2300k
NASA/SP-8057, Structural Design Criteria Applicable to a Space Shuttle, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), March, 1972, pp. 99, Format(s): PDF 7231k
NASA/SP-8058, Spacecraft
Aerodynamic Torques, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance And Control),
NASA (Washington, DC, United States), January, 1971, pp. 37, Format(s): PDF
1760k
Assessment of
disturbance torques due to interaction of spacecraft with atmosphere in long
duration orbits for use in design of spacecraft attitude control systems.
NASA/SP-8059, Spacecraft attitude control during thrusting maneuvers, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance And Control), NASA (Washington, DC, United States), February, 1971, pp. 51, Format(s): PDF 2970k
NASA/SP-8060, Compartment venting, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), November, 1970, pp. 31, Format(s): PDF 1748k
NASA/SP-8061,
Anschicks*, R.D., Interactions with umbilicals and launch stand, NASA SPACE
VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States),
*Martin Marietta, August, 1970, pp. 23, Format(s): PDF 1208k
Criteria and
recommendations to ensure compatible interfaces between space vehicle structure
and launch stand ground support equipment.
NASA/SP-8062, Sherman*,
M.M., Entry gasdynamic heating, NASA SPACE VEHICLE DESIGN CRITERIA
(Structures), NASA (Washington, DC, United States), NASA Langley Research
Center (Hampton, VA, United States), *Philco-Ford Corporation, January, 1971,
pp. 60, Format(s): PDF 3339k
Determining
heat transfer to space vehicles entering planetary atmospheres for proper design
and thermal protection.
NASA/SP-8063, Jones*, J.R., Lubrication friction and wear, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), *Hughes Aircraft Co. (Canoga Park, CA, United States), June, 1971, pp. 180, Format(s): PDF 4350k
NASA/SP-8064, Solid propellant selection and characterization, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA (Washington, DC, United States), June, 1971, pp. 116, Format(s): PDF 13245k
NASA/SP-8065, Tubular
spacecraft booms (extendible, reel stored), NASA SPACE VEHICLE DESIGN CRITERIA
(Guidance), NASA (Washington, DC, United States), June, 1971, pp. 52,
Format(s): PDF 5887k
Development of reliable and operational design programs for spacecraft guidance and control.
NASA/SP-8066, Deployable
aerodynamic deceleration systems, NASA SPACE VEHICLE DESIGN CRITERIA
(Structures), NASA Langley Research Center (Hampton, VA, United States),
June, 1971, pp. 88, Format(s): PDF 9694k
Criteria and
recommended practices for design, selection, analysis, and testing of
deployable aerodynamic deceleration systems.
NASA/SP-8067, Earth
albedo and emitted radiation, NASA SPACE VEHICLE DESIGN CRITERIA (Environment),
NASA (Washington, DC, United States), July, 1971, pp. 48, Format(s): PDF 4761k
Global annual
averages f earth albedo and radiation used to estimate long term effects on
space vehicle equipment and surfaces.
NASA/SP-8068, Buckling strength of structural plates, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), June, 1971, pp. 50, Format(s): PDF 5226k
NASA/SP-8069, Divine,
N., The planet Jupiter (1970), NASA SPACE VEHICLE DESIGN CRITERIA
(Environment), NASA (Washington, DC, United States), December, 1971, pp.
93, Format(s): PDF 10014k
Data obtained
through 1970, some materials published during the first half of 1971, and
conclusions of the Jupiter Radiation Belt Workshop held in July 1971 are
presented.
NASA/SP-8070, Spaceborne
digital computer systems, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance),
NASA (Washington, DC, United States), March, 1971, pp. 82, Format(s): PDF
10187k
Design criteria
for guidance and control spaceborne computer selection including physical and
functional characteristics and reliability.
NASA/SP-8071, Passive gravity-gradient libration dampers, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance), NASA (Washington, DC, United States), February, 1971, pp. 60, Format(s): PDF 3518k
NASA/SP-8072, Acoustic loads generated by the propulsion system, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), June, 1971, pp. 54, Format(s): PDF 2629k
NASA/SP-8073, Solid
propellant grain structural integrity analysis, NASA SPACE VEHICLE DESIGN
CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United
States), June, 1973, pp. 114, Format(s): PDF 6357k
The structural
properties of solid propellant rocket grains were studied to determine the
propellant resistance to stresses. Grain geometry, thermal properties,
mechanical properties, and failure modes are discussed along with design criteria
and recommended practices.
NASA/SP-8074, Spacecraft solar cell arrays, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA (Washington, DC, United States), May, 1971, pp. 54, Format(s): PDF 3374k
NASA/SP-8075, Solid propellant processing factor in rocket motor design, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA (Washington, DC, United States), October, 1971, pp. 82, Format(s): PDF 5242k
NASA/SP-8076, Solid
propellant grain design and internal ballistics, NASA SPACE VEHICLE DESIGN
CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United
States), March, 1972, pp. 110, Format(s): PDF 6701k
The ballistic
aspects of grain design were studied to outline the steps necessary to achieve
a successful grain design. The relationships of the grain design to
steady-state mass balance and erosive burning are considered. Grain design
criteria is reviewed, and recommended design criteria are included.
NASA/SP-8077, Ostrem, F.E., Transportation and handling loads, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA Langley Research Center (Hampton, VA, United States), September, 1971, pp. 48, Format(s): PDF 3035k
NASA/SP-8078, Spaceborne electronic imaging systems, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance), NASA (Washington, DC, United States), June, 1971, pp. 71, Format(s): PDF 4257k
NASA/SP-8079, Noll*, R. B. and Zvara*, J., Structural interaction with control systems , NASA Langley Research Center (Hampton, VA, United States), *Aerospace Systems Inc., November, 1971, pp. 56, Format(s): PDF 3255k
NASA/SP-8080, Liquid rocket pressure regulators, relief valves, burst disks, and explosive valves, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA (Washington, DC, United States), March, 1973, pp. 123, Format(s): PDF 7268k
NASA/SP-8081, Liquid propellant gas generators, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), March, 1972, pp. 110, Format(s): PDF 11723k
NASA/SP-8082, Stress-corrosion cracking in metals, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA Langley Research Center (Hampton, VA, United States), August, 1971, pp. 42, Format(s): PDF 4970k
NASA/SP-8083, Discontinuity stresses in metallic pressure vessels, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA Langley Research Center (Hampton, VA, United States), August, 1971, pp. 69, Format(s): PDF 5595k
NASA/SP-8084, Surface
atmospheric extremes (launch and transportation areas), NASA SPACE VEHICLE
DESIGN CRITERIA (Environment), NASA Marshall Space flight Center
(Huntsville, AL, United States), January, 1974, pp. 77, Format(s): PDF 7030k
Criteria are
provided on atmospheric extremes from the surface to 150 meters for
geographical locations of interest to NASA. Thermal parameters (temperature and
solar radiation), humidity, precipitation, pressure, and atmospheric
electricity (lightning and static) are presented. Available data are also
provided for the entire continental United States for use in future space
programs.
NASA/SP-8085, The planet Mercury (1971), NASA SPACE VEHICLE DESIGN CRITERIA (Environment), NASA (Washington, DC, United States), March, 1972, pp. 63, Format(s): PDF 5873k
NASA/SP-8086, Space
vehicle displays design criteria, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical),
NASA (Washington, DC, United States), March, 1972, pp. 45, Format(s): PDF 5453k
The guidance, navigation, and control displays associated with manned spaceflight are summarized. Major emphasis were placed on methodologies useful for determining necessary information and its uses, systems analysis techniques, and analytic methods for design and evaluation of such systems.
NASA/SP-8087, Liquid
rocket engine fluid-cooled combustion chambers, NASA SPACE VEHICLE DESIGN
CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United
States), April, 1972, pp. 120, Format(s): PDF 12865k
A monograph on
the design and development of fluid cooled combustion chambers for liquid
propellant rocket engines is presented. The subjects discussed are (1)
regenerative cooling, (2) transpiration cooling, (3) film cooling, (4)
structural analysis, (5) chamber reinforcement, and (6) operational problems.
NASA/SP-8088, Wagner, W.
A., Liquid rocket metal tanks and tank components, NASA SPACE VEHICLE DESIGN
CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United
States), May, 1974, pp. 165, Format(s): PDF 16716k
Significant
guidelines are presented for the successful design of aerospace tanks and tank
components, such as expulsion devices, standpipes, and baffles. The state of
the art is reviewed, and the design criteria are presented along with
recommended practices. Design monographs are listed.
NASA/SP-8090, Liquid rocket actuators and operators, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), May, 1973, pp. 158, Format(s): PDF 17926k
NASA/SP-8091, The
planet Saturn (1970), NASA SPACE VEHICLE DESIGN CRITERIA (Environment),
NASA (Washington, DC, United States), June, 1972, pp. 103, Format(s): PDF 6035k
The present-day
knowledge on Saturn and its environment are described for designers of
spacecraft which are to encounter and investigate the planet.
NASA/SP-8092, Assessment
and control of spacecraft electromagnetic interference, NASA SPACE VEHICLE
DESIGN CRITERIA (Environment), NASA Goddard Space Flight Center (Greenbelt,
MD, United States), June, 1972, pp. 37, Format(s): PDF 2176k
Assessment and control of spacecraft electromagnetic interference.
Design criteria are presented to provide guidance in assessing electromagnetic
interference from onboard sources and establishing requisite control in
spacecraft design, development, and testing.
NASA/SP-8093, Solid rocket motor internal insulation, NASA SPACE VEHICLE DESIGN CRITERIA (Environment), NASA (Washington, DC, United States), December, 1976, Format(s): PDF 2100k
NASA/SP-8094, Liquid
rocket valve components, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical),
NASA Lewis Research Center (Cleveland, OH, United States), August, 1973, pp.
150, Format(s): PDF 8668k
A monograph on
valves for use with liquid rocket propellant engines is presented. The
configurations of the various types of valves are described and illustrated.
Design criteria and recommended practices for the various valves are explained.
Tables of data are included to show the chief features of valve components in
use on operational vehicles.
NASA/SP-8095, Preliminary
criteria for the fracture control of space shuttle structures, NASA SPACE VEHICLE
DESIGN CRITERIA (Environment), NASA (Washington, DC, United States), June,
1971, pp. 16, Format(s): PDF 967k
Preliminary criteria for the fracture control of space shuttle structures. The complex and multidisciplinary factors are presented which relate to the prevention of structural failure due to the initiation or propagation of cracks or crack-like defects.
NASA/SP-8096, Space
vehicle gyroscope sensor applications, NASA SPACE VEHICLE DESIGN CRITERIA
(Guidance), NASA (Washington, DC, United States), June, 1972, pp. 87,
Format(s): PDF 4960k
Considerations
which form the basis for the specification, design and evaluation of gyroscopes
for spaceborne sensor applications are presented.
NASA/SP-8097, Liquid
rocket valve assemblies, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical),
NASA Lewis Research Center (Cleveland, OH, United States), November, 1973, pp.
154, Format(s): PDF 8985k
The design and
operating characteristics of valve assemblies used in liquid propellant rocket
engines are discussed. The subjects considered are as follows: (1) valve
selection parameters, (2) major design aspects, (3) design integration of valve
subassemblies, and (4) assembly of components and functional tests. Information
is provided on engine, stage, and spacecraft checkout procedures.
NASA/SP-8098, Effects
of structural flexibility on entry vehicle control systems, NASA SPACE VEHICLE
DESIGN CRITERIA (Guidance), NASA (Washington, DC, United States), June,
1972, pp. 68, Format(s): PDF 4254k
Control
system/structure interactions of space vehicles during planetary and earth
entry were investigated with principal emphasis on atmospheric entry and
aerodynamic deceleration to subsonic speeds.
NASA/SP-8099, Houbolt,
J. C., Combining ascent loads, NASA SPACE VEHICLE DESIGN CRITERIA
(Structures), NASA (Washington, DC, United States), June, 1972, pp. 36,
Format(s): PDF 1597k
Criteria
and guidelines are presented for combining loads that develop during the ascent
phase of a space flight. The primary load-caring structure is discussed
including the basic tank and interconnecting members, engine support mounts and
connections to tank structure, transition structures between stages, payload
shrouds, and the basic support points at separation planes.
NASA/SP-8100, Liquid
rocket engine turbopump gears, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical),
NASA Lewis Research Center (Cleveland, OH, United States), March, 1974, pp.
117, Format(s): PDF 5495k
Design
and fabrication of gear drives for rocket engine turbopumps are described in
the sequence encountered during the design process as follows: (1) selection of
overall arrangement; (2) selection of gear type; (3) preliminary sizing; (4)
lubrication system design; (5) detail tooth design; (6) selection of gear
materials; and (7) gear fabrication and testing as it affects the design. The
description is oriented towards the use of involute spur gears, although
reference material for helical gears is also cited.
NASA/SP-8101, Liquid
rocket engine turbopump shafts and couplings, NASA SPACE VEHICLE DESIGN
CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United
States), September, 1972, pp. 130, Format(s): PDF 13343k
Design criteria
and recommended practices are presented for designing tubopump shafts and
couplings. Design parameters, material selection, and structural analysis are
discussed.
NASA/SP-8102, Space
vehicle accelerometer applications, NASA SPACE VEHICLE DESIGN CRITERIA
(Guidance), NASA (Washington, DC, United States), December, 1972, pp. 87,
Format(s): PDF 4904k
The physics of
accelerometer applications are reviewed, and details are given on accelerometer
instruments and the principles of their operations.
NASA/SP-8103, Palluconi,
F. D., The planets Uranus, Neptune, and Pluto (1971), NASA SPACE VEHICLE DESIGN
CRITERIA (Environment), NASA Goddard Space Flight Center (Greenbelt, MD,
United States), November, 1972, pp. 99, Format(s): PDF 5410k
Design criteria
relating to spacecraft intended to investigate the planets of Uranus, Neptune,
and Pluto are presented.
NASA/SP-8104, Structural interaction with transportation and handling systems, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), January, 1973, pp. 41, Format(s): PDF 2200k
NASA/SP-8105, Spacecraft
thermal control, NASA SPACE VEHICLE DESIGN CRITERIA (Environment), NASA
(Washington, DC, United States), May, 1973, pp. 48, Format(s): PDF 2497k
Guidance for
the assessment and control of spacecraft temperatures is provided with emphasis
on unmanned spacecraft in the space environment. The heat balance, elements of
thermal design, and thermal control are discussed along with thermal testing,
design criteria, and recommended practices.
NASA/SP-8107, Turbopump
systems for liquid rocket engines, NASA SPACE VEHICLE DESIGN CRITERIA
(Chemical), NASA Lewis Research Center (Cleveland, OH, United States), August,
1974, pp. 168, Format(s): PDF 9814k
The turbopump
system, from preliminary design through rocket engine testing is examined.
Selection of proper system type for each application and integration of the
components into a working system are dealt with. Details are also given on the
design of various components including inducers, pumps, turbines, gears, and
bearings.
NASA/SP-8108, Advanced composite structures, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA Langley Research Center (Hampton, VA, United States), August, 1974, pp. 107, Format(s): PDF 5711k
NASA/SP-8109, Liquid
rocket engine centrifugal flow turbopumps, NASA SPACE VEHICLE DESIGN CRITERIA
(Chemical), NASA Lewis Research Center (Cleveland, OH, United States),
December, 1973, pp. 116, Format(s): PDF 5847k
Design criteria
and recommended practices are discussed for the following configurations
selected from the design sequence of a liquid rocket engine centrifugal flow
turbopump: (1) pump performance including speed, efficiency, and flow range;
(2) impeller; (3) housing; and (4) thrust balance system. Hydrodynamic,
structural, and mechanical problems are addressed for the achievement of
required pump performance within the constraints imposed by the engine/turbopump system. Materials and
fabrication specifications are also discussed.
NASA/SP-8110, Liquid
rocket engine turbines, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA
Lewis Research Center (Cleveland, OH, United States), January, 1974, pp. 158,
Format(s): PDF 8105k
Criteria for
the design and development of turbines for rocket engines to meet specific performance,
and installation requirements are summarized. The total design problem, and
design elements are identified, and the current technology pertaining to these
elements is described. Recommended practices for achieving a successful design
are included.
NASA/SP-8111, Barrett,
M., Assessment and control of electrostatic charges, NASA SPACE VEHICLE
DESIGN CRITERIA (Environment), NASA Goddard Space Flight Center (Greenbelt,
MD, United States), May, 1974, pp. 53, Format(s): PDF 2652k
The experience is described of NASA and DOD with electrostatic
problems, generation mechanisms, and type of electrostatic hazards. Guidelines
for judging possible effects of electrostatic charges on space missions are
presented along with mathematical formulas and definitions.
NASA/SP-8112, Pressurization systems for liquid rockets, NASA SPACE VEHICLE DESIGN CRITERIA,
October, 1975, Format(s): PDF 7700k
Guidelines for the successful design of pressurization systems for main
propulsion, auxiliary propulsion, and attitude control systems for boosters,
upper stages, and spacecraft were presented, drawing on the wealth of design
experience that has accumulated in the development of pressurization systems
for liquid rockets operational in the last 15 years.
NASA/SP-8113, Liquid
rocket engine combustion stabilization devices, NASA SPACE VEHICLE DESIGN
CRITERIA (Chemical), NASA (Washington, DC, United States), November, 1974,
pp. 127, Format(s): PDF 8241k
Combustion
instability, which results from a coupling of the combustion process and the
fluid dynamics of the engine system, was investigated. The design of devices
which reduce coupling (combustion chamber baffles) and devices which increase
damping (acoustic absorbers) are described.
NASA/SP-8114, Solid rocket thrust vector control, NASA SPACE VEHICLE DESIGN CRITERIA (Chemical), NASA Lewis Research Center (Cleveland, OH, United States), December, 1974, pp. 200, Format(s): PDF 20758k
This
page was compiled and kindly provided to me by Phil Martin. Lukas
Ströbel kindly provided updated links and abstracts.