TY - JOUR
T1 - CRYOGENIC PROPELLANT MANAGEMENT - INTEGRATION OF DESIGN, PERFORMANCE AND OPERATIONAL REQUIREMENTS.
AU - Worlund, Armis L.
AU - Jamieson, John R.
AU - Cole, Timothy W.
AU - Lak, Tibor I.
PY - 1985/1/1
Y1 - 1985/1/1
N2 - The integration of some of the unique design features of the Shuttle elements into a cryogenic propellant management system is described. The implementation and verification of the design/operational changes resulting from design deficiencies and/or element incompatibilities encountered subsequent to the critical design reviews are emphasized. Major topics include subsystem designs to provide liquid oxygen (LO//2) tank pressure stabilization, LO//2 facility vent for ice prevention, liquid hydrogen (LH//2) feedline high point bleed, pogo suppression on the Space Shuttle Main Engine (SSME), LO//2 low level cutoff, Orbiter/engine propellant dump, and LO//2 main feedline helium injection for geyser prevention. (Author abstract. )
AB - The integration of some of the unique design features of the Shuttle elements into a cryogenic propellant management system is described. The implementation and verification of the design/operational changes resulting from design deficiencies and/or element incompatibilities encountered subsequent to the critical design reviews are emphasized. Major topics include subsystem designs to provide liquid oxygen (LO//2) tank pressure stabilization, LO//2 facility vent for ice prevention, liquid hydrogen (LH//2) feedline high point bleed, pogo suppression on the Space Shuttle Main Engine (SSME), LO//2 low level cutoff, Orbiter/engine propellant dump, and LO//2 main feedline helium injection for geyser prevention. (Author abstract. )
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M3 - Conference article
AN - SCOPUS:0021975521
SP - 585
EP - 599
JO - NASA Conference Publication
JF - NASA Conference Publication
SN - 0191-7811
IS - pt 2
ER -