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  • SPACECRAFT DESIGN, TESTING AND PERFORMANCE  (5)
  • Cell & Developmental Biology
  • General Chemistry
  • 1975-1979  (9)
  • 1
    Electronic Resource
    Electronic Resource
    New York, NY [u.a.] : Wiley-Blackwell
    Journal of Cellular Physiology 93 (1977), S. 335-344 
    ISSN: 0021-9541
    Keywords: Life and Medical Sciences ; Cell & Developmental Biology
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology , Medicine
    Notes: Various biochemical properties of mitochondria isolated from primary monolayer cultures of mammary epithelial cells from mid-pregnant or hormonally stimulated mice were examined daily for seven or eight days. When compared with mitochondria from mammary glands of mid-pregnant animals, the specific activities of several mitochondrial enzymes were greatly reduced in cells after seven days in culture. There was a 5- to 6-fold reduction in the specific activities of cytochrome oxidase, succinate dehydrogenase and α glycerophosphate oxidase while malate dehydrogenase and adenylate kinase activities were 2- to 3-fold lower. The reduction in mitochondrial enzyme activities was gradual and related to the length of time the cells were in culture. Progressive changes were also seen in the electrophoresis profiles of mitochondrial proteins in SDS-urea polyacrylamide gels. Mitochondria isolated from 1-, 2-, 3- and 8-day cell cultures showed a continuous reduction in the relative amounts of several mitochondrial polypeptides in the gel profiles. Addition of 35S-methionine to cell cultures for short and long periods indicated that mitochondrial protein synthesis continued throughout the 8-day culture period. However, the synthesis of several particular polypeptides was reduced progressively during the culture period. These studies indicate that mouse mammary epithelial cells have a lowered capacity for respiratory metabolism as a result of specific mitochondrial alterations which might be associated with the general loss of differentiated morphology by those cells during monolayer culture.
    Additional Material: 4 Ill.
    Type of Medium: Electronic Resource
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  • 2
    Electronic Resource
    Electronic Resource
    New York, NY [u.a.] : Wiley-Blackwell
    Journal of Cellular Physiology 99 (1979), S. 441-450 
    ISSN: 0021-9541
    Keywords: Life and Medical Sciences ; Cell & Developmental Biology
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Biology , Medicine
    Notes: We have studied the effects of theophylline treatment on pigmentation characteristics and growth of two B16 melanoma cell lines, HFH-18 and P/140. Cell counts of control and theophylline-treated cultures confirmed that the drug inhibits cell growth. Light and electron microscope cytochemistry with the L-dopa reaction indicated that the two cell lines differ in their ability to transfer Golgi-associated tyrosinase to developing premelanosomes. The results of these experiments, considered with results of electrophoretic analyses and activity measurements by the Pomerantz method, also provide evidence that increased tyrosinase synthesis occurs in response to theophylline treatment. In addition, results indicate that theophylline induces changes in the rate of synthetic or degradative posttranslational modification of tyrosinase. Measurements of intracellular cyclic AMP levels by radioimmunoassay in control cultures and in theophylline- and α-MSH-treated cultures were made. Although the hormone induced spectacular increases in cyclic AMP levels, theophylline produced no detectable change. These results indicate that theophylline differs from α-MSH because theophylline-induced changes in pigmentation may not require the participation of intracellular cyclic AMP.
    Additional Material: 6 Ill.
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  • 3
    ISSN: 0044-8249
    Keywords: Chemistry ; General Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Additional Material: 1 Ill.
    Type of Medium: Electronic Resource
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  • 4
    ISSN: 0570-0833
    Keywords: Chemistry ; General Chemistry
    Source: Wiley InterScience Backfile Collection 1832-2000
    Topics: Chemistry and Pharmacology
    Additional Material: 1 Ill.
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  • 5
    Publication Date: 2019-06-27
    Description: For abstract, see N76-18209.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-144183 , LMSC-HREC-TR-D496644
    Format: application/pdf
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  • 6
    Publication Date: 2019-06-27
    Description: Preliminary designs and the supporting analysis for both the Aeromaneuvering Orbit-to-Orbit Shuttle (AMOOS) and the Aeromaneuvering Recovery System (AMRS) are presented. The AMOOS design is shown to yield from twice to almost three times the high energy, round-trip payloads as a purely propulsive vehicle of the same weight. Typically AMOOS can perform a crew rotation mission to equatorial geosynchronous orbit in one space shuttle launch. The flight test program analysis modeled parameters such as maximum dynamic pressure, heating rates, guidance, stability and recovery. Two model flight schedules were developed, one consisting of four flights and the other of two flights. The former is considered a very low risk, high information return program whereas the latter is a minimal cost program consistent with reasonable data returns and chance of success. The AMOOS and AMRS guidance scheme developed using linear regulator theory proved a precise and accurate guidance scheme. Both it and a classical linear system's based scheme were evaluated using 65 simulated trajectories in which the position in the entry corridor and the atmospheric density were varied randomly.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: NASA-CR-144182 , LMSC-HREC-TR-D496705
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  • 7
    Publication Date: 2019-06-27
    Description: The drag characteristics of the space shuttle orbiter thermal protection system (TPS) tiles were studied experimentally in subsonic flow. Full-scale tiles were mounted to a 3.05 x 3.5 m test board in four configurations plus a completely smooth case. Pressure gradients were produced by tilting the board relative to the freestream. The drags due to steps, slots, and gaps between the tiles were evaluated at various orientations, pressure gradients, and Reynolds numbers. Results showed that the contribution of gaps and slots were minor compared to those of typical steps. The results for skin friction did not correlate as a fully rough surface. Thus, the surface area of the TPS tiles was sufficient to allow smooth-wall Reynolds number effects even though the steps between tiles could double the skin friction.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: Journal of Spacecraft and Rockets; 14; Mar. 197
    Format: text
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  • 8
    Publication Date: 2019-07-13
    Description: The steady-state matrix Ricatti equation is studied with respect to sensitivity and computational burden for a linear regulator controller in spacecraft. The class of systems studied use control moment gyros (CMGs) as the torque driver, assuming that the CMGs are free of gimbal stops. Different solution techniques are evaluated relative to computation time and accuracy to determine which solution method is most acceptable with respect to the prescribed requirements. It is shown that it is not feasible to eliminate off-diagonal Ricatti equation terms in the relevent updata equation due to their high sensitivity, that Potter's algebraic technique requires the least computation time of the methods studied, and that the simple Euler method yields the best results when accuracy and computation time are equally weighted. If an optimal linear regulator formulation is employed, a full Ricatti equation solution of n(n + 1)2 elements of the symmetric positive definite gain matrix which is the solution to the matrix Ricatti equation must be computed at each update cycle.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AIAA PAPER 76-157 , Aerospace Sciences Meeting; Jan 26, 1976 - Jan 28, 1976; Washington, DC
    Format: text
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  • 9
    Publication Date: 2019-07-13
    Description: The thermostructural response of three candidate carbon-carbon composites for the Jovian entry probe heatshield was investigated. The analysis for the three materials, Sandia Felt, Carbitex 700, and SAI 4-D weave carbon-carbon was conducted using a dual finite element approach which involved heat conduction as well as the structural response. A receding boundary due to ablation and inertial loads encountered by the probe were included. Severe cracking, circumferential and radial, and interlaminar shear failure was observed during the radiative heating pulse for the Sandia Felt and Carbitex 700 materials, respectively. The 4-D weave material showed no failures over the entire entry.
    Keywords: SPACECRAFT DESIGN, TESTING AND PERFORMANCE
    Type: AIAA PAPER 79-0920 , Conference on Advanced Technology for Future Space Systems; May 08, 1979 - May 10, 1979; Hampton, VA
    Format: text
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