The Microgravity Research Experiments (MICREX) Database


Capillarity


Equilibrium Shift Reaction/Chemical Foaming


Principal Investigator(s):

Grodzka, P. G. (1); Facemire, B. R. (2)

Co-Investigator(s):

Unknown

Affiliations:

(1) During ASTP: Lockheed Missiles and Space Company, Inc., Huntsville, Alabama, Currently: Faratech, Inc., Huntsville, Alabama; (2) National Aeronautics and Space Administration (NASA) Marshall Space Flight Center (MSFC), Huntsville, Alabama

Experiment Origin:

United States of America

Mission:

Apollo-Soyuz Test Project (ASTP)

LaunchDate/Experiment Date:

07/15/75

Launched From:

NASA Kennedy Space Center, Florida

Payload Type:

Science Demonstration, ASTP Manned Environment

Processing Facility:

Foaming solutions were initiated into test tubes via syringes

Builder of Processing Facility:

Unknown

Experiment Summary:

Equilibrium Shift Reaction/Chemical Foaming

"A foam consists of bubbles of gas encased by walls of thin liquid films. Although some foams can be made rigid or flexible and durable, the characteristic foam is not stable on Earth. Foams collapse primarily as a result of the gravity-induced drainage of liquid in the bubble walls. As the liquid drains from the bubble, the film walls become increasingly thin until, at a thickness of approximately 10 nanometers (100 angstroms), they are ruptured by random molecular motion. Thus, the foam gradually dissipates as more of the liquid drains away to bulk form and leaves less to support the bubble walls. In the zero-g environment of space, drainage is substantially reduced; therefore, a longer lasting foam is provided. Drainage, however, is only one of the mechanisms contributing to the dissipation of foams. Evaporation and liquid spreading also act to dissipate bubble walls. Thus, the full extent of foam stability is still uncertain.

"Forming a foam in space yields a very large surface area-to-volume ratio of the liquid that should be retained for a relatively long period. This large, stable surface area should enable surface-sensitive chemical reactions to occur differently than they would on Earth. The sensitivity of some chemical reactions to the size of the interface area has long been known....However, the precise change taking place at the interface has not been precisely determined, and definitive theories on the characteristics of a stable foam in space have not been generated. Nevertheless, it was anticipated that a chemical reaction dependent on the surface area of the air-to-liquid interface... would proceed differently in a foam in a zero-g environment than would normally occur on Earth." (3, pp. 31-2 - 31-3)

This experiment was one of two chemical foam science demonstrations designed by Grodzka et al. performed during the ASTP mission. (See Grodzka, ASTP, "The Formaldehyde Clock Reaction/Chemical Foaming" to review the other experiment.) The specific objective of the Equilibrium Shift Reaction Experiment was to visually demonstrate the stability of foams under low-gravity conditions.

Prior to the initiation of the experiment, it appears that two Lexan test tubes were each filled with a gold-colored solution comprised of (1) 10.7 mg thymol blue, (2) 10 ml ethyl alcohol, (3) 0.2 cc concentrated hydrochloric acid, and (4) 500 ml distilled water. (Thymol blue of pH 2.8 will turn from brown amber to pink when foamed by shaking.)

During the ASTP experiment, a crew member shook the tubes and the resulting pink foams were recorded on motion picture film. The contrast of the brightly colored pink foam against the gold bulk solution was clearly visible to the crewman as the foam dissipated.

It was reported that (a) the foams created under low-gravity conditions were very stable while those foams created on Earth collapsed within a few seconds, and (b) because the "...16 millimeter motion picture was out of focus, detailed knowledge of the foam dissipation [time] in the pink foam has not been determined." (3, p. 31-4)

No other results from this experiment were reported.

Key Words:

*Capillarity*Foams*Foam Stability*Aqueous Solutions*Liquid Mixing*Bubbles*Bubble Dispersion*Surface Tension*Liquid Spreading*Thin Films*Fluid Drainage*Interface Physics*Evaporation*Contained Fluids*Liquid/Gas Dispersion*Liquid/Gas Interface*Solid/Liquid Interface*

Number of Samples:

two

Sample Materials:

A solution comprised of: (1) thymol blue, (2) water, (3) ethyl alcohol, and (4) hydrochloric acid

Container Materials:

Lexan test tubes

Experiment/Material Applications:

"Foams are currently used in such diverse applications as the separation of proteins by the fractionation of foams and the origination of rigid structures such as foamed polystyrene and foam rubber. It has been suggested... that such unique products as reinforced rigid foams could be formed in space without the influence of gravity. In such foams, metal fibers would be alined [sic] along the surface of a stable foam strictly by adhesion. When cured, the foam could have a light-weight durability possibly unknown with earthbound processes. It has also been suggested that space-originated foams could act as the basis of porous metal electrodes. Such new products and synthesis procedures are potential applications of foam technology in space." (3, p. 31-3)

References/Applicable Publications:

(1) Grodzka, P.: Three Model Space Experiments on Chemical Reactions. Proc. of the 1976 NASA Colloquium on Bioprocessing in Space, Houston, Texas, March 10-12, 1976, NASA TM X-58191, pp. 67-76. (post-flight)

(2) Grodzka, P. and Facemire, B.: Chemical Reactions in Low-G. American Institute of Aeronautics and Astronautics 16th Aerospace Sciences Meeting, Huntsville, Alabama, January 16-18, 1978, 5 pp. (post-flight)

(3) Snyder, R. S., Clifton, K. S., Facemire, B., Whitaker, A. F., Grodzka, P. G., and Bourgeois, S.: Science Demonstrations. In Apollo-Soyuz Test Project--Preliminary Science Report, NASA TM X-58173, February 1976, pp. 31-1 - 31-9. (post-flight)

(4) Grodzka, P. G. and Bourgeois, S. V.: The Apollo Soyuz Science Demonstration Experiments; Final Report. Lockheed Missiles and Space Company, Inc., LMSC-HREC-TR-D497499, October 1977, work performed under NASA/MSFC Contract NAS8-32222.

(5) Naumann, R. J. and Mason, E. D.: Chemical Foams. In Summaries of Early Materials Processing in Space Experiments, NASA TM-78240, August 1979, p. 72. (post-flight)

Contact(s):

Philomena G. Grodzka
Faratech, Inc.
526 Clearmont Drive SE
Huntsville, AL 35801

Barbara Facemire
ES76
NASA Marshall Space Flight Center, AL 35812