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At least 1,135 records · Page 63

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NASA NTRS1972

The earth orbit shuttle as a space rescue vehicle.

According to present concepts starting with some future date all manned space missions beyond low-earth orbit are to originate in low-earth orbit and to return ultimately to low-earth orbit. The Earth-Orbit-Shuttle (EOS) is visualized as the only vehicle operating between earth and low-earth orbit. The ability of the EOS to provide rescue services in the case of emergency is evaluated. It is found that an employment of the EOS as rescue vehicle is basically feasible, although it has certain limitations. Complementary means of transportation are required for emergencies beyond low-earth orbit. Approaches to enhance the rescue mission utility of the EOS are discussed.

Hinton, M. G., Jr.↗

NASA NTRS1971

External fuel thermionic reactor system.

Thermionic reactors are prime candidates for nuclear electric propulsion. The national thermionic reactor effort is concentrated on the flashlight concept with the external-fuel concept as the backup. The external-fuel concept is very adaptable to a completely modular power subsystem which is attractive for highly reliable long-life applications. The 20- to 25-cm long, externally-fueled converters have been designed, fabricated, and successfully tested with many thermal cycles by electrical heating. However, difficulties have been encountered during encapsulation for nuclear heated tests and none have been started to date. These nuclear tests are required to demonstrate the concept feasibility.

Mondt, J. F.↗

NASA NTRS1972

Moonquakes and lunar tectonism.

Review of the major discoveries that have resulted to date from the analysis of seismic data from a network of geophysical stations on the moon. It is found that lunar seismic signals differ greatly from typical terrestrial seismic signals; the moon possesses a crust and a mantle, at least in the region of the Apollo 12 and 14 stations; natural lunar events detected by the Apollo seismic network are moonquakes and meteoroid impacts; and in addition to the repeating moonquakes, moonquake 'swarms' have been discovered.

Latham, G.↗

NASA NTRS1972

Lunar neutron stratigraphy.

Study of the isotopic composition of gadolinium and samarium in four soil and seven drill stem samples returned by the Apollo 15 mission. The results show the possibility to date sedimentary processes on the lunar surface for time scales of around 100 million years because of the particular dependence of neutron capture reactions on depth. The neutron flux has a distinct peak as a function of depth. This peak appears to lie below the level of shallow cratering for time scales of less than one billion years and consequently forms a readily identified marker layer of both depth and time.

Russ, G. P., III↗

NASA NTRS1972

An integrated computer system for preliminary design of advanced aircraft.

A progress report is given on the first phase of a research project to develop a system of Integrated Programs for Aerospace-Vehicle Design (IPAD) which is intended to automate to the largest extent possible the preliminary and detailed design of advanced aircraft. The approach used is to build a pilot system and simultaneously to carry out two major contractual studies to define a practical IPAD system preparatory to programing. The paper summarizes the specifications and goals of the IPAD system, the progress to date, and any conclusion reached regarding its feasibility and scope. Sample calculations obtained with the pilot system are given for aircraft preliminary designs optimized with respect to discipline parameters, such as weight or L/D, and these results are compared with designs optimized with respect to overall performance parameters, such as range or payload.

Fulton, R. E.↗

NASA NTRS1972

About the interaction between a satellite and its environmental ionospheric plasma.

Results from recent in situ observations performed by electron probes on board the Explorer XXXI satellite are combined with earlier Ariel I and Explorer VIII results to yield a more complete and up to date picture of the structure of the near wake of an ionospheric satellite. Various aspects of the interaction between a spacecraft and its environmental spaceplasma are discussed. Avenues for future experimental work are briefly mentioned.

Samir, U.↗

NASA NTRS1972

Mariner Venus-Mercury 1973 encounter strategy.

This paper describes the selection of launch and arrival conditions and Venus and Mercury encounter aiming zones to maximize the science return from the Mariner Venus-Mercury mission. A single Mariner spacecraft will be launched in November, 1973, fly by Venus in early February, 1974, and encounter Mercury (the primary target) in late March, 1974. Mercury aiming points will provide: (1) sun and earth occultation, (2) 1000 km periapsis altitude, and (3) return to Mercury after 176 days (two Mercury years). The selected Mercury arrival dates allow high-contrast television imaging. Aiming points at Venus allow gravity assist to Mercury and also permit earth occultation.

Shirley, D. L.↗

NASA NTRS1972

Effects of weightlessness on astronauts - A summary.

This paper reviews the adaptive changes observed in the United States astronauts during flight programs to this date. A series of postulates are offered as to what is happening in these adaptive events. A hypothesis is proposed as to the interrelationship of events observed in the body systems and functions involved. The importance of undertaking an extensive life sciences program, including an on-orbit phase of study as well as pre- and post-flight studies is discussed. Finally, the role the Skylab flight plays in the United States Space Program in achieving the future requirements for more extensive life sciences data is summarized.

White, S. C.↗

NASA NTRS1972

The lunar conductivity profile and the nonuniqueness of electromagnetic data inversion.

A review of the theory for the electromagnetic functional used to date to determine the lunar conductivity profile from spectral analyses of lunar magnetometer data. The 'hard' boundary condition used by Sonett et al. (1971) and others appears to be a good approximation for the sunlit lunar hemisphere. The use of the spectral data in conjunction with the functional to find a least squares conductivity profile is examined from the point of view of the nonuniqueness of nonlinear estimation. An unsuccessful search was carried out to find models that were both geophysically reasonable and consistent with the data. It is asserted that the failure to find these models is due to the inadequacy of the functional. Of the models generated, those that best fit the data all have a conductivity peak at a depth of 240 km similar to that of the model discussed by Sonett et al. However, all of these models are quite distinct elsewhere in the profile. It is shown how such models are dependent on both the nature of the functional as well as the initial guess in the least squares procedure. A correlation analysis shows that the only resolvable features from this type of model are a low conductivity crust, a high conductivity peak of limited radial extent, and a low conductivity zone beneath the peak.

Phillips, R. J.↗

NASA NTRS1972

Experiments leading to the production of new glasses in space.

Report on an experimental program aimed at verifying proposed concepts of glassmaking in space from substances that to date have been observed only in a crystalline condition. A summary is presented on the results of experiments conducted by laser melting of ceramic rods of chosen composition and allowing the droplets ejected from the spinning rod to cool by free falling. This technique should permit an early evaluation of which compositions are most suitable for subsequent more expensive space experiments.

Happe, R. A.↗

NASA NTRS1972

The determination of the satellite orbit of Mariner 9.

This paper presents a comprehensive analysis of the Mars orbital phase of the Mariner 9 trajectory as determined from Earth based radio data. Both the method and accuracy of the orbit determination process are reviewed. Analysis is presented to show the effects of Mars gravity model and node in the plane of the sky errors on the accuracy of orbit determination. In addition the long term evolution of the orbit from insertion to date is presented, and is decomposed into effects from the Mars gravity field, n-body perturbations, and solar radiation pressure. Since the orbit period is nearly commensurable with the Mars rotational period, the orbit experiences significant resonance perturbations. The primary perturbation is in-track with a maximum amplitude of 1000 km and a wavelength of 39 revolutions.

Born, G. H.↗

NASA NTRS1973

GREMEX update (Goddard research engineering management exercise)

Management simulation techniques offer training in management problems. Exercise was developed to provide experience in research and development project decision making from management rather than technological perspective. Program and documentation have been revised innumerable times in past. Described report is revised version as it exists to date.

Vaccaro, M. J.↗

NASA NTRS1973

Materials data handbooks on aluminum alloys

Five handbooks have been prepared which describe up-to-date properties of the following wrought-aluminum alloys: 2014, 2219, 5456, 6061, and 7075. Each handbook is divided into twelve chapters. Scope of information presented includes physical- and mechanical-property data at cryogenic, ambient, and elevated temperatures.

Muraca, R. F.↗

NASA NTRS1972

A hybrid computer program for the visual display of compensatory system model parameters

A hybrid computer identification program has been developed which determines and displays those parameter values of a model of the compensatory control system that existed over the last fifteen seconds of operation. These values are up-dated every 0.05 sec so that a visual display of the parameters appears to be continuous. Presently, a closed loop crossover model is being used as the compensatory system model with the parameters K and tau displayed, however, any suitable model could be used in its place.

Jackson, G. A.↗

NASA NTRS1972

Adaption of a corrector module to the IMP dynamics program

The corrector module of the RAEIOS program and the IMP dynamics computer program were combined to achieve a date-fitting capability with the more general spacecraft dynamics models of the IMP program. The IMP dynamics program presents models of spacecraft dynamics for satellites with long, flexible booms. The properties of the corrector are discussed and a description is presented of the performance criteria and search logic for parameter estimation. A description is also given of the modifications made to add the corrector to the IMP program. This includes subroutine descriptions, common definitions, definition of input, and a description of output.

Source record↗

NASA NTRS1972

Explicit expressions of the potential and its derivatives at the origin in terms of the scattering data

The quantum mechanical theory of scattering of a particle by a spherically symmetrical potential is presented. As in the inverse scattering problem, the input of the calculation is the scattering and bound-state data, and the output is data on the potential. The results discussed are explicit expressions for the values of the potential and its derivatives at the origin in terms of the scattering and boundstate data. Various methods to obtain these results are outlined. The presentation is aimed at introducing these various approaches. The simplest scattering problem (nonrelativistic S-wave scattering on a holomorphic potential without bound states) is used as the basis for discussion, and technicalities are omitted whenever possible without loss of clarity. A complete compilation is given of the results obtained to date in this field, including the treatment of higher partial waves and the Klein-Gordon and Dirac equations.

Calogero, F.↗

NASA NTRS1972

Sonic inlet development for turbofan engines

The static program has shown to date that very large noise reductions can be achieved by the sonic inlet concept with realistic inlet length and good aerodynamic performance. It is also shown that different inlet concepts produce substantially different results.

Klujber, F.↗

NASA NTRS1972

Use of satellite imagery for wildland resource evaluation

The author has identified the following significant results. Accurate identification and delineation of crested wheatgrass seedlings has enabled a broad inventory of this resource. The entire state of Nevada is being inventoried for crested wheatgrass seedlings. Irrigated fields and pastures are easily visible from ERTS-1 imagery and were quantified in total acres on 12,500 square miles of the state. Recent fire scars may be monitored and inventoried from satellite-borne imagery. Inventory and quantification of large native meadows of Nevada have been accomplished on one frame of ERTS-1 data. This inventory would not have been economically feasible with any known ground inventory method. The U-2 sequential data taken in the spring revealed several resource management oriented phenological changes in the vegetation. The green-up of grasses and shrubs was detected on the imagery and supplied a good indicator for livestock turn-out dates. Water level manipulations in the Ruby Marsh were readily detected by noting changes in vegetation growth and reflectance.

Tueller, P. T.↗