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  • ASTRODYNAMICS  (5)
  • genotypic variation  (2)
  • 1
    Electronic Resource
    Electronic Resource
    Springer
    Plant and soil 155-156 (1993), S. 513-516 
    ISSN: 1573-5036
    Keywords: Lupinus ; genotypic variation ; root growth ; alkalinity
    Source: Springer Online Journal Archives 1860-2000
    Topics: Agriculture, Forestry, Horticulture, Fishery, Domestic Science, Nutrition
    Notes: Abstract Commercial lupins grow poorly on alkaline and neutral fine-textured soils. Genotypic variation exists among lupins. The present study compared the growth of 13 lupin genotypes, including introduced cultivars and wild types, in an alkaline loamy soil and an acid loamy soil. Plants grown in the alkaline and acid soils did not show obvious symptoms of iron deficiency at any stage. There was however a large variation of shoot fresh weight among genotypes in response to the alkaline soil with L. atlanticus and L. pilosus being more tolerant than L. luteus, L. cosentinii, L. albus and L. angustifolius. Some variation also existed among genotypes of L. angustifolius. In addition, root growth was retarded on the alkaline soil except for L. atlanticus, L. pilosus P20955 and L. albus Kiev mutant. In the alkaline soil, root growth at week 2 correlated well with the shoot fresh weight at week 12. The results suggest that early root elongation may be useful for screening tolerant genotypes for alkaline soils.
    Type of Medium: Electronic Resource
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  • 2
    Electronic Resource
    Electronic Resource
    Springer
    Plant and soil 186 (1996), S. 321-330 
    ISSN: 1573-5036
    Keywords: adaptation ; bicarbonate ; genotypic variation ; grain legumes ; pH
    Source: Springer Online Journal Archives 1860-2000
    Topics: Agriculture, Forestry, Horticulture, Fishery, Domestic Science, Nutrition
    Notes: Abstract Defining plant adaptation to soil conditions is critical for the successful introduction of grain legume species into farming systems. This nutrient solution study examined the effects of pH (4, 5, 6, 7 and 8) and bicarbonate (5 mM KHCO3) on the growth and nodulation of 14 grain legume species supplied with N or reliant on N2-fixation. Species includedPisum sativum L.,Cicer arietinum L.,Lens culinaris Med., and a range ofLupinus, Vicia andLathyrus species. Species differed greatly in response to solution pH. For both N-fertilized and N2-fixing plants, shoot growth ofL. culinaris was very sensitive to low pH (pH 〈 7), whereas shoot growth ofLupinus angustifolius L. andLupinus albus L. was sensitive to higher pH (pH ≥ 6). Other species had a broader optimal pH range for growth when supplied with N, but were generally sensitive to low pH (pH 〈 7 forC. arietinum andVicia sativa L., pH 〈 6 forP. sativum, Vicia faba L.,Lathyrus sativus L. andLathyrus cicera L., and pH 〈 5 forVicia benghalensis L. andVicia narbonensis L.) when reliant on N2-fixation. For these other species, symbiotic N2-fixation appeared to be more sensitive than host plant growth to low pH. This finding was supported by lower nodule numbers and mass, and lower N concentrations in shoots of sensitive species at low pH relative to higher pH. ForL. culinaris, nodule numbers and mass were relatively unaffected by pH 5–8, N concentrations in shoots were high at low pH and plants developed symptoms relating to H+ toxicity at pH as high as 7. These results indicate that host plant growth ofL. culinaris is more sensitive to low pH than theRhizobium symbiosis. ForL. albus andL. angustifolius, both host plant growth and symbiotic N2-fixation appeared to be equally sensitive to pH ≥ 6.Lupinus pilosus Murr. was more tolerant of high pH than the otherLupinus species. At pH 4, two genotypes ofC. arietinum had better early nodulation than other species.Vicia ervilia L. nodulated poorly at all levels of solution pH, indicating that the commercial Group E inoculum (Rhizobium leguminosurum bv.viceae SU303) may not be effective for this species in solution culture. Addition of bicarbonate decreased shoot growth, nodulation and N concentrations in shoots of most species. Early nodulation (nodule number) ofLathyrus ochrus (L.) DC was not affected by the bicarbonate treatment.
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  • 3
    Publication Date: 2019-06-28
    Description: By a three-dimensional Lagrangian formulation, an exact set of ten coupled nonlinear second-order differential equations has been derived for a system with an extensible tether connecting two end satellites of distributed mass. The effects of tether mass, small orbital eccentricity, central body oblateness, aerodynamic drag force, and solar radiation pressure are also included in the formulation. By linearizing the exact differential equations, the in-plane (orbital plane) differential equations are found to be decoupled from the out-of-plane ones. The characteristic equation of the in-plane differential equations is derived and some associated stability constraints are shown.
    Keywords: ASTRODYNAMICS
    Type: AAS PAPER 85-340
    Format: text
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  • 4
    Publication Date: 2019-06-28
    Description: This paper presents the concise exact solution for predicting view-periods to be observed from a masked or unmasked tracking station on a tri-axial ellipsoidal surface. The new exact approach expresses the azimuth and elevation angles of a spacecraft in terms of the station-centered geodetic topocentric coordinates in an elegantly concise manner. A simple and efficient algorithm is developed to avoid costly repetitive computations in searching for neighborhoods near the rise and set times of each satellite orbit for each station. Only one search for each orbit is necessary for each station. Sample results indicate that the use of an assumed spherical earth instead of an 'actual' tri-axial ellipsoidal earth could introduce an error up to a few minutes in a view-period prediction for circular orbits of low or medium altitude. For an elliptical orbit of high eccentricity and long period, the maximum error could be even larger. The analytic treatment and the efficient algorithm are designed for geocentric orbits, but they should be applicable to interplanetary trajectories by an appropriate coordinates transformation at each view-period calculation. This analysis can be accomplished only by not using the classical orbital elements.
    Keywords: ASTRODYNAMICS
    Type: AIAA PAPER 86-2068
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  • 5
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    In:  Other Sources
    Publication Date: 2019-07-13
    Description: The autonomous (or unmanned) Mars Orbit Rendezvous may be divided into four phases: approach, terminal, station-keeping, and docking. The paper outlines a feasible concept for the terminal rendezvous phase. A co-apsidal terminal rendezvous technique is described which utilizes the advantages of aligning the lines of apsides of two coplanar elliptic orbits of slightly different periods but of the same apoapsis distance. An initial maneuver nulling the inclination between the orbits is followed by another maneuver to align the two lines of apsides. A proper phasing maneuver is then executed at the coapsidal point, and the final rendezvous maneuver is performed at the same coapsidal point to complete the terminal rendezvous transfer. Cases are formulated in order of complexity with a view to illustrate the basic ideas of this technique. Pertinent calculations are also presented.
    Keywords: ASTRODYNAMICS
    Type: AAS PAPER 79-167 , American Astronautical Society and American Institute of Aeronautics and Astronautics, Astrodynamics Specialist Conference; Jun 25, 1979 - Jun 27, 1979; Provincetown, MA
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  • 6
    Publication Date: 2019-06-28
    Description: A preliminary study of an all-sky coverage of the EUVE mission is given. Algorithms are provided to compute the exposure of the celestial sphere under the spinning telescopes, taking into account that during part of the exposure time the telescopes are blocked by the earth. The algorithms are used to give an estimate of exposure time at different ecliptic latitudes as a function of the angle of field of view of the telescope. Sample coverage patterns are also given for a 6-month mission.
    Keywords: ASTRODYNAMICS
    Type: AIAA PAPER 84-2017
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  • 7
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    In:  Other Sources
    Publication Date: 2019-07-13
    Description: Aerobraking techniques are applied to trajectory design for the VOIR (Venus Orbiting Imaging Radar) mission to enhance overall mission performance. The approach can be used for other planetary missions such as a Titan orbiter or a Mars sample return to earth. The orientation of the elliptical insertion orbit must be chosen in such a way that the combined effects of solar gravity, central-body harmonics, and drag on periapsis altitude are minimized to avoid frequent maneuvers. The selection of the base and width of a corridor for periapsis altitude depends upon the temperature and integrated heat of the aerobrake shield, the atmospheric density profile, the duration of aerobraking, the number of maneuvers, the time available between maneuvers, and uncertainties in the central-body gravity field and atmospheric density. Flight path profiles for an aerodynamically stable spacecraft and an inertially fixed spacecraft passing through the free molecular flow regime, as well as the transitional flow regime, are illustrated
    Keywords: ASTRODYNAMICS
    Type: AAS PAPER 81-132 , Astrodynamics Specialist Conference; Aug 03, 1981 - Aug 05, 1981; Lake Tahoe, NV; US
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