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SHIVA (Spaceflight Holography Investigation in a Virtual Apparatus)This paper provides the description and results of a ground-based experiment designed to support the spaceflight program SHIVA, which started its flight definition in 1998. SHIVA will apply new diagnostic tools and experimental techniques to test the validity of a newly discovered analytical solution to the general equation of motion of a particle in a fluid. We have designed a spaceflight experiment with the help of the theoretical model that is optimized for testing the model, and for measuring g, g-jitter, and other microgravity phenomena. Our ongoing, ground-based particle/fluid experiment supports both the experimental and theoretical aspects of the project. The ultimate spaceflight experiment will be similar to the ground-based experiment. The "virtual spaceflight chamber" concept asserts that certain spaceflight experiments can be recorded in holograms in such a manner that having the holograms on earth is optically equivalent to being back in space with unlimited time to conduct the experiment. Properly exploited, this concept can save a significant amount of experiment time in space by effectively bringing the. experiment optically back to earth. SHIVA will accomplish the following: record a large number of holograms of particle fields in space under controlled conditions, extract the precise, three-dimensional position of all of the particles as a function of time, examine the effects of all parameters on the motion of the particles, and test these against predictions of the Coimbra-Range1 solution to the general equation of motion. Particle sizes will range from hundreds of microns up to about 2 mm in diameter and will cover a range of densities and fluid viscosities. Forcing functions will be introduced onto the particle field, including at least the following: a) No isolation in the Spacelab vibration environment. b) Isolation from Spacelab. c) Oscillatory motion from 1 to 100 Hz with amplitudes of a few millimeters. d) Convective fields to be introduced mechanically. The first objective of this research is to understand the physics of particle interactions with fluids and other particles in low Reynolds number flows in microgravity. Secondary objectives are to: (1) observe and quantify g-jitter effects and microconvection on particles in fluids, (2) validate an exact solution to the general equation of motion of a particle in a fluid, and (3) to characterize'the ability of isolating platforms to isolate experiments containing particles in liquids.
Document ID
20090011903
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Trolinger, James D.
(MetroLaser Irvine, CA, United States)
Witherow, William
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rogers, Jan
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rangel, Roger
(California Univ. Irvine, CA, United States)
Coimbra, Carlos
(Drexel Univ. Philadelphia, PA, United States)
Date Acquired
August 24, 2013
Publication Date
July 8, 2000
Subject Category
Space Sciences (General)
Meeting Information
Meeting: International Symposia on Applications of Laser Techniques to Fluid Mechanics
Location: Lisbon
Country: Portugal
Start Date: July 8, 2000
Distribution Limits
Public
Copyright
Public Use Permitted.
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