"IU/S-IVB Forward Skirt Orbital and Translunar Thermal Analyses."

"IU/S-IVB Forward Skirt Orbital and Translunar Thermal Analyses."

This report determines the maximum and minimum solar and terrestrial thermal energy incident and absorbed by Saturn IB/V vehicles in earth orbit and translunar travel. The influence' of this external energy on the Instrument Unit Thermal Conditioning System performance, and consequently its ade...

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Bibliographic Details
Main Author: Huneidi, F.
Other Authors: George C. Marshall Space Flight Center. Fluid Mechanics and Thermodynamics Branch Propulsion Division
Format: Electronic
Published: University of Alabama in Huntsville Archives
Subjects:
Documents
Online Access:http://libarchstor2.uah.edu/digitalcollections/items/show/10923
format Electronic
collection Saturn V Collection
building University of Alabama in Huntsville Archives
publisher University of Alabama in Huntsville Archives
topic Documents
spellingShingle Documents
"IU/S-IVB Forward Skirt Orbital and Translunar Thermal Analyses."
Huneidi, F.
fulltopic Documents
Saturn project
Electronic instruments
Instrumentation
Saturn launch vehicles
Cooling systems
description This report determines the maximum and minimum solar and terrestrial thermal energy incident and absorbed by Saturn IB/V vehicles in earth orbit and translunar travel. The influence' of this external energy on the Instrument Unit Thermal Conditioning System performance, and consequently its adequacy to maintain the electronic packages at acceptable temperature limits is ascertained. Conclusions are: a) Methanol/water coolant temperature will deviate from 111 specifications only during translunar cold flights. However, adequate thermal conditioning of the electronic equipment would still be maintained. b) Instrument Unit missions exceeding 6 1/2 hours, or electronic packages heat dissipation magnitudes lower than 3 kw or higher than 8.5 kw, should be reviewed to ascertain thermal compatibility.
spelling "IU/S-IVB Forward Skirt Orbital and Translunar Thermal Analyses."Huneidi, F.George C. Marshall Space Flight Center. Fluid Mechanics and Thermodynamics Branch Propulsion DivisionSaturn projectElectronic instrumentsInstrumentationSaturn launch vehiclesCooling systemsThis report determines the maximum and minimum solar and terrestrial thermal energy incident and absorbed by Saturn IB/V vehicles in earth orbit and translunar travel. The influence' of this external energy on the Instrument Unit Thermal Conditioning System performance, and consequently its adequacy to maintain the electronic packages at acceptable temperature limits is ascertained. Conclusions are: a) Methanol/water coolant temperature will deviate from 111 specifications only during translunar cold flights. However, adequate thermal conditioning of the electronic equipment would still be maintained. b) Instrument Unit missions exceeding 6 1/2 hours, or electronic packages heat dissipation magnitudes lower than 3 kw or higher than 8.5 kw, should be reviewed to ascertain thermal compatibility.1966-01-13TextReportsiusivbforskiorbandtratheana.pdfspc_stnv_000350http://libarchstor2.uah.edu/digitalcollections/items/show/10923http://libarchstor2.uah.edu/digitalcollections/files/original/20/10923/iusivbforskiorbandtratheana_081707134156.pdfSaturn V CollectionBox 16, Folder 4University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabamaenspc_stnv_000350_000374This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections.
title "IU/S-IVB Forward Skirt Orbital and Translunar Thermal Analyses."
titleStr "IU/S-IVB Forward Skirt Orbital and Translunar Thermal Analyses."
author Huneidi, F.
author_facet Huneidi, F.
George C. Marshall Space Flight Center. Fluid Mechanics and Thermodynamics Branch Propulsion Division
author2 George C. Marshall Space Flight Center. Fluid Mechanics and Thermodynamics Branch Propulsion Division
id UAHsaturnv10923
url http://libarchstor2.uah.edu/digitalcollections/items/show/10923
_version_ 1790443372049072129

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