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  • 1
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    Empirical solar proton model for orbiting spacecraft applications (1974)
    In:  Other Sources
    Details
    Publication Date: 2011-08-16
    Description: An empirical model for energetic solar proton fluxes is presented. With this model the effects of such protons on geocentric space missions, to be flown during the next solar active period (1977-1983), and with orbits involving partial magnetospheric shielding, may be estimated. A synoptic background review is given, followed by a detailed discussion of the model's use, errors, uncertainties, and limitations, including sample calculations which demonstrate the application of specific or general project missions. Finally, for circular trajectories, percentage exposure maps are presented, depicting fractional mission times spent outside particular L shells as functions of orbit altitude and inclination.
    Keywords: SPACE RADIATION
    Type: IEEE Transactions on Aerospace and Electronic Systems; AES-10; July 197
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    Solar proton fluences for 1977-1983 space missions (1974)
    In:  Other Sources
    Details
    Publication Date: 2011-08-16
    Description: The probability with which any given solar proton fluence level will be exceeded during a space mission is computed for mission to be flown during the active phase of the next solar cycle (1977-1983). This probability is a function of fluence level, proton energy threshold, and mission duration. Calculations are based on 1966-1972 data only. In estimating mission fluences, a distinction is made between ordinary and anomalously large events. Probable numbers of each type of event are estimated from Burrell's extension of Poisson statistics. Fluences of all anomalously large events are assumed to have a spectrum given by the August 1972 event, while fluences of the ordinary events are assumed to obey a log normal distribution.
    Keywords: SPACE RADIATION
    Type: Journal of Spacecraft and Rockets; 11; June 197
    Format: text
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  • 3
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    Solar radio burst and in situ determination of interplanetary electron density (1983)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A few interplanetary electron density scales which were derived from the analysis of interplanetary solar radio burst are discussed and compared to a model derived from 1974 to 1980 Helios 1 and 2 in situ density observations made in the 0.3 to 1.0 AU range. The Helios densities were normalized to 1976 with the aid of IMP and ISEE data at 1 AU, and were then sorted into 0.1 AU bins and logarithmically averaged within each bin. The best fit to these 1976-normalized, bin averages is N(R(AU)) = 6.1 R(-2.10)/cu cm. This model is in rather good agreement with the solar burst determination if the radiation is assumed to be on the second harmonic of the plasma frequency. This analysis also suggests that the radio emissions tend to be produced in regions denser than the average where the density gradient decreases faster with distance than the observed R(-2.10).
    Keywords: SPACE RADIATION
    Type: NASA-TM-85094 , NAS 1.15:85094
    Format: application/pdf
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  • 4
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    Energetic solar proton versus terrestrially trapped proton fluxes for the active years 1977 - 1983 (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: Ratios of solar to trapped proton fluences were computed for circular-orbit, geocentric space missions to be flown during the active phase of the next solar cycle (1977-1983). The ratios are presented as functions of orbit altitude and inclination, mission duration, proton energy threshold, and the chance the mission planner is willing to take that the actually encountered solar proton fluence will exceed the design fluence provided by the statistical solar proton model. It is shown that the ratio is most sensitively dependent on orbit altitude and inclination, with trapped protons dominant for low inclination, low and mid altitude orbits and for high inclination, mid altitude orbits. Conversely, solar protons are dominant for high inclination, low altitude orbits, and for low and high inclination, high altitude orbits.
    Keywords: SPACE RADIATION
    Type: NASA-TM-X-70716 , X-601-74-221
    Format: application/pdf
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  • 5
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    Solar proton fluences as observed during 1966-1972 and as predicted for 1977-1983 space missions (1973)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: The probability with which any given proton fluence level will be exceeded during a space mission is computed for missions to be flown during the active phase of the next solar cycle (1977-1983). This probability is a function of fluence level, proton energy threshold, and mission duration. Data on the major solar proton events of 1966-1972 are given; it is argued that only this data set (and not that of the previous solar cycle) is appropriate for estimating next-cycle fluences. Probable numbers of each of the two types of events are estimated from Burrell's extension of Poisson statistics. Fluences of all future anomalously large events are assumed to have a common spectrum, that given by the August 1972 event. Fluences of the ordinary events are assumed to obey a log normal distribution. It is shown that for much of the confidence-level mission-duration regime of interest, at least one anomalously large event will occur; and given such an occurrence, the ordinary-event contribution to mission fluence is negligible.
    Keywords: SPACE RADIATION
    Type: NASA-TM-X-70508 , X-601-73-324
    Format: application/pdf
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  • 6
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    An empirical model of energetic solar proton fluxes with applications to earth orbiting spacecraft (1972)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: An empirical model for energetic solar proton fluxes is presented. With this model, the effects of such protons on geocentric space missions, to be flown during the next solar active period (1966-1983) and with orbits involving partial magnetospheric shielding, may be estimated. A synoptic background review is given, followed by a detailed discussion of the model's analytic development. Also given are comments on the model's use, errors, uncertainties, and limitations, including sample calculations which demonstrate the application of specific or general project missions. Finally, for circular trajectories, percentage exposure maps are presented, depicting fractional mission times spent outside particular L-shells as functions of orbit altitude and inclination.
    Keywords: SPACE RADIATION
    Type: NASA-TM-X-70433 , X-601-72-489
    Format: application/pdf
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