Paper
27 April 1988 Superfluid Helium Orbital Resupply: The Status Of The SHOOT Flight Experiment And Preliminary User Requirements
Michael J DiPirro, Peter Kittel
Author Affiliations +
Abstract
The Superfluid Helium On-Orbit Transfer (SHOOT) Flight Experiment is designed to demonstrate the components and techniques necessary to resupply superfluid helium to satellites or space station based facilities. A top level description as well as the development status of the critical components to be used in SHOOT are discussed. Some of these components include the thermomechanical pump, the fluid acquisition system, the normal helium and superfluid helium phase separators, venturi flow meter, cryogenic valves, burst disks, and astronaut compatible extra vehicular activity (EVA) coupler and transfer line. The requirements for the control electronics and software are given. A preliminary description of the requirements that must be met by a satellite requiring superfluid helium servicing are given. In particular, minimum and optimum plumbing arrangements are shown, transfer line flow impedance and heat input impacts are assessed, instrumentation described, and performance parameters considered.
© (1988) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Michael J DiPirro and Peter Kittel "Superfluid Helium Orbital Resupply: The Status Of The SHOOT Flight Experiment And Preliminary User Requirements", Proc. SPIE 0973, Cryogenic Optical Systems and Instruments III, (27 April 1988); https://doi.org/10.1117/12.948334
Lens.org Logo
CITATIONS
Cited by 2 scholarly publications.
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Liquids

Helium

Cryogenics

Receivers

Electronics

Optical cryogenics

Sensors

Back to Top