NDLI: Task 4 supporting technology. densification requirements definition and test objectives. propellant densification requirements definition

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Task 4 supporting technology. densification requirements definition and test objectives. propellant densification requirements definition

Content Provider	NASA Technical Reports Server (NTRS)
Author	Lak, Tibor Weeks, D. P.
Copyright Year	1995
Description	The primary challenge of the X-33 CAN is to build and test a prototype LO2 and LH2 densification ground support equipment (GSE) unit, and perform tank thermodynamic testing within the 15 month phase 1 period. The LO2 and LH2 propellant densification system will be scaled for the IPTD LO2 and LH2 tank configurations. The IPTD tanks were selected for the propellant technology demonstration because of the potential benefits to the phase 1 plan: tanks will be built in time to support thermodynamic testing; minimum cost; minimum schedule risk; future testing at MSFC will build on phase 1 data base; and densification system will be available to support X-33 and RLV engine test at IPTD. The objective of the task 1 effort is to define the preliminary requirements of the propellant densification GSE and tank recirculation system. The key densification system design parameters to be established in Task 1 are: recirculation flow rate; heat exchanger inlet temperature; heat exchanger outlet temperature; maximum heat rejection rate; vent flow rate (GN2 and GH2); densification time; and tank pressure level.
File Size	29567522
Page Count	22
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19950021839
Archival Resource Key	ark:/13960/t51g5mt1w
Language	English
Publisher Date	1995-05-30
Access Restriction	Open
Subject Keyword	Thermodynamics And Statistical Physics Propellant Storage Thermodynamics Densification Inlet Temperature Liquid Oxygen Liquid Rocket Propellants Flow Velocity Ground Support Equipment Heat Exchangers Propellant Tanks Liquid Hydrogen Reusable Launch Vehicles Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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