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ACME

OVERVIEW

ACME is focused on advanced combustion technology via fundamental microgravity research. The primary goal is to improve efficiency and reduce pollutant emission in practical terrestrial combustion. A secondary objective is fire prevention, especially for spacecraft.

Currently, ACME includes five independent experiments (see ACME Experiments below) investigating laminar, gaseous, non-premixed flames.

The ACME experiments will be conducted with a single modular set of hardware (see ACME Implementation) in the Combustion Integrated Rack (CIR) on the International Space Station (ISS).

An ACME precursor, Structure & Liftoff In Combustion Experiment (SLICE), was conducted in the ISS’ Microgravity Science Glovebox (MSG) in early 2012.

The ACME design is complete and the engineering hardware is being assembled for integrated testing. On-orbit testing is expected to begin in 2016 and continue for a few years.

ACME STATUS

January 2015-

ACME’s Phase II Safety Review was held in Houston on Oct. 7-8, 2014.

The ACME engineering hardware was assembled and recently underwent preliminary integrated testing with the Ground Integration Unit (GIU) for the Combustion Integrated Rack (CIR).  The engineering hardware is now set up for testing in NASA Glenn’s Electromagnetic Interference Laboratory (i.e., for EMI).

Nearly 60 prototype spherical burners were fabricated for the Flame Design and s-Flame experiments, including 22 bronze burners from GKN Sinter Metals Filters GmbH, 8 stainless steel burners from Mott Corp., and 27 bronze burners from Princeton University.  Evaluation testing has begun in NASA Glenn’s 2.2 Second Drop Tower to determine if they will produce microgravity flames that are sufficiently spherical.

Evaluation testing of a 25-mm diameter prototype BRE burner was completed, where a total of 35 drops were conducted in NASA Glenn’s Zero Gravity Research Facility (from Feb.-Nov. 2014).  Similar evaluation has now begun a 50-mm BRE burner.

Six presentations were given by ACME researchers at the 2014 meeting of the American Society of Gravitational and Space Research (ASGSR).  One of the six, “Implementation of High Dynamic Range (HDR) Image Algorithms for Improved Microgravity Flame Diagnostics” by David Giassi (Yale University) et al., was also presented as a student poster and received honorable mention recognition.

The initial results of the CLD Flame precursor experiment, Structure & Liftoff In Combustion Experiment (SLICE) have now been published.  The papers were both presented at the 35th International Symposium on Combustion (San Francisco, CA; 3-8 August, 2014), where preliminary versions had been presented at the 8th U.S. National Combustion Meeting (Park City, UT; 19-22 May, 2013).

Bin Ma, Su Cao, Davide Giassi, Dennis P. Stocker, Fumiaki Takahashi, Beth Anne V. Bennett, Mitchell D. Smooke, and Marshall B. Long, “An experimental and computational study of soot formation in a coflow jet flame under microgravity and normal gravity,” Proceedings of the Combustion Institute, Volume 35, Issue 1, 2015, Pages 839–846.

S. Cao, B. Ma, B.A.V. Bennett, D. Giassi, D.P. Stocker, F. Takahashi, M.B. Long, and M.D. Smooke, “A computational and experimental study of coflow laminar methane/air diffusion flames: Effects of fuel dilution, inlet velocity, and gravity,” Proceedings of the Combustion Institute, Volume 35, Issue 1, 2015, Pages 897–903.

Left:  Spherical flame from just before impact in a drop test in the 2.2 Second Drop Tower, where the dim flame image was brightened in post processing.  In this test, a mixture of 30/70 ethylene/nitrogen (on a volume basis) flowed from the 6.35-mm diameter spherical burner into ambient air at atmospheric pressure.  The bright glow is the hot-wire igniter which was deactivated but not retracted during the drop.

Right: BRE flame from near the end of a drop test in the Zero Gravity Research Facility.  In this test, a mixture of 50/50 ethylene/nitrogen (on a volume basis) flowed from the 25-mm diameter burner into a 26/74 oxygen/nitrogen atmosphere at 0.8 atm.  With this atmosphere, the normal oxygen partial pressure (i.e., 0.21 atm) has been maintained.

Finally, an updated list of ACME Publications and Presentations is now available online.

ACME NUMBERS 3, 5, 8, 11

3 payload developers: ZIN Technologies, Inc., NASA, and the National Center for Space Exploration Research (NCSER).

5 current ACME experiments (see below).

8 universities with which ACME investigators have been affiliated, but where investigator Prof. Felix J. Weinberg of Imperial College London regrettably died in 2012. There are also ACME investigators from the NASA Glenn Research Center, which is the agency’s lead for microgravity combustion research.

11 current investigators for the ACME experiments.

ACME LOGO

LargeACMElogo

ACME EXPERIMENTS

(listed alphabetically)

Burning Rate Emulator (BRE)

Objective: Fire Safety- To improve our fundamental understanding of materials flammability, such as extinction behavior and the conditions needed for sustained combustion, and to assess the relevance of existing flammability test methods for low and partial-gravity environments.
Flame/Burner: Flat perforated disk fed with gaseous fuel to simulate the burning of solid and liquid fuels, where measurements are made of the thermal feedback upon which the vaporization of such fuels depend.
Principal Investigator: Prof. James G. Quintiere, University of Maryland
Co-Investigator: Prof. Peter B. Sunderland, University of Maryland

Coflow Laminar Diffusion Flame (CLD Flame)

Objective: Energy & Environment – To extend the range of flame conditions that can be accurately predicted by computational models, especially for highly dilute and heavily sooting conditions.
Flame/Burner: Coflow flame where the gaseous fuel issues from an inner tube which is centered within a much larger outer tube, where a mixture of oxygen and nitrogen issues from the annulus.
Principal Investigator: Prof. Marshall B. Long, Yale University
Co-Investigator: Prof. Mitchell D. Smooke, Yale University

Electric-Field Effects on Laminar Diffusion Flames (E-FIELD Flames)

Objective: Energy & Environment – To gain an improved understanding of ion production in flames and investigate how an electric field can be used to control flames through those ions.
Flame/Burner: Gas-jet flame, where (1) the gaseous fuel issues from a small circular tube into a still atmosphere, and (2) a high-voltage electric field is established between the burner and disk-shaped copper mesh centered a few centimeters “above” the burner. Electric-field tests may also be conducted with the coflow burner used for the CLD Flame experiment.
Principal Investigator: Prof. Derek Dunn-Rankin, University of California – Irvine

Flame Design

Objective: Energy & Environment – To improve our understanding of soot inception and control in order to enable the optimization of oxygen-enriched combustion and the “design” of non-premixed flames that are both robust and soot free.
Flame/Burner: Spherical flame – which is only possible in microgravity – where the burner gas (fed through a small tube) issues from a porous spherical burner. Tests are planned for both (1) normal flames, where the fuel flows into an oxygen/inert atmosphere, and (2) inverse flames, where an oxygen/inert mixture flows into a fuel atmosphere.
Principal Investigator: Prof. Richard L. Axelbaum, Washington University in St. Louis
Co-Investigators: (1) Prof. Beei-Huan Chao, University of Hawaii; (2) Prof. Peter B. Sunderland, University of Maryland; (3) Dr. David L. Urban, NASA Glenn Research Center

Structure and Response of Spherical Diffusion Flames (s-Flame)

Objective: Energy & Environment – To advance our ability to predict the structure and dynamics, including extinction, of both soot-free and sooty flames.
Flame/Burner: Spherical flame – which is only possible in microgravity – where the gaseous fuel (fed through a small tube) issues from a porous spherical burner into a still atmosphere.
Principal Investigator: Prof. C.K. Law, Princeton University
Co-Investigators: (1) Prof. Stephen D. Tse, Rutgers University; (2) Dr. Kurt R. Sacksteder, NASA Glenn Research Center

ACME BENEFITS & RELEVANCE

Why study combustion?

In the United States, nearly 70% of our electrical energy is generated through the combustion of fossil fuels. For example, in 2012, electricity was generated in the U.S. by burning the following fuels, where the percentages indicate the fraction of the total U.S. electrical generation: coal (37%), natural gas (30%), biomass (1.4%), and petroleum (1%).

Our transportation is heavily reliant on combustion, even for electric vehicles because most of our electricity is generated by combustion.

With combustion, we heat our homes, water, food, etc. and also generate heat for industrial processes.

Our reliance on imported fuel contributes to our national trade deficit and affects our national security.

Combustion is a leading man-made source of greenhouse gases, where carbon dioxide is the most important example.

Combustion is the primary man-made contributor to acid rain.

Soot contributes to global warming and is a health problem.

Fire safety!

Given our pervasive use of combustion as an energy source, the U.S. consumes fossil fuels which cost on the order of a trillion dollars annually. Therefore, even small improvements in combustion efficiency would significantly reduce fuel needs and pollutant production.

Why study combustion in microgravity?

Flames are strongly affected by gravity because the high-temperature combustion gases are much less dense than the cooler atmosphere which surrounds the flame. Gravity pulls more forcefully on the denser atmosphere and the hot gases are pushed upward as a result. This gravity-driven upward motion of material that is less dense that the surrounding fluid is referred to as buoyancy. This gravity-driven motion, referred to as buoyant convection, feeds the flame with fresh reactant – normally oxygen (in the air) – and removes the combustion products (e.g., carbon dioxide and water vapor) from the flame vicinity.

Low-momentum flames are dramatically influenced by the effective elimination of buoyant convection, where the resulting effects are often advantageous for analysis.

Spherically symmetric flames can be created enabling one-dimensional analysis. Two of the current ACME experiments take advantage of this feature.

Flicker, which is a buoyancy-driven (i.e., gravity-driven) instability, is eliminated yielding quasi-steady flames.

Length scales are increased in microgravity flames facilitating analysis of the flame structure.

Momentum-dominated flames, which are important for most practical combustion, can be studied at low velocities to simplify analysis.

Microgravity flames tend to have a much stronger sensitivity to their atmosphere and exhibit a much broader range of characteristics than normal-gravity flames because of the near absence of buoyant entrainment.

The long residence times in microgravity flames can lead to strong soot production, but many microgravity flames are soot free.

Microgravity flames are great for studies of limit and stability behavior where chemical kinetics are important. Soot, extinction, and stability limits are being studied in the ACME experiments.

Microgravity is of course the appropriate environment for studies related to spacecraft fire safety.

Why study combustion on the ISS?

Microgravity durations in drop facilities, such as the 2.2 Second Drop Tower and 5.18-second Zero Gravity Research Facility, are (1) too short for soot to achieve quasi-steady conditions, and (2) too short to establish a flame and then vary its flow rate, for example, to investigate stability or extinction limits.

While research aircraft flying in parabolic maneuvers can provide reduced gravity durations of ~20 seconds, low-momentum flames are often dramatically disturbed by the aircraft vibrations. Although the jitter can be avoided if the experiment is floated within the aircraft, that reduces the low-gravity duration to mere seconds.

Space-based testing is often necessary to achieve microgravity conditions of sufficient duration and quality for combustion research.

ACME STATUS ARCHIVE

July 2014 – Two papers (listed below) on the ACME precursor experiment, Structure & Liftoff In Combustion Experiment (SLICE), will be presented at this summer’s 35th International Symposium on Combustion.
B. Ma, S. Cao, D. Giassi, D.P. Stocker, F. Takahashi, B.A.V. Bennett, M.D. Smooke, and M.B. Long, “An experimental and computational study on soot formation in a coflow jet flame under microgravity and normal gravity,” to be presented, 35th International Symposium on Combustion, San Francisco, CA, 3-8 August, 2014.
S. Cao, B. Ma, B.A.V. Bennett, D. Giassi, D.P. Stocker, F. Takahashi, M.B. Long, and M.D. Smooke, “A computational and experimental study of coflow laminar methane/air diffusion flames: Effects of fuel dilution, inlet velocity, and gravity,” to be presented, 35th International Symposium on Combustion, San Francisco, CA, 3-8 August, 2014.

SLICE was conducted on the International Space Station in early 2012 to prepare for ACME’s Coflow Laminar Diffusion Flame (CLD Flame) experiment. CLD Flame is led by Yale professors Marshall Long and Mitch Smooke, whose combined experimental and computational research (including SLICE) is described in the 2012 Yale Engineering magazine’s cover story. Two ACME posters will also be presented at the symposium:

D.P. Stocker, F. Takahashi, J.M. Hickman, and A.C. Suttles, “Advanced Combustion via Microgravity Experiments: Planned International Space Station Research on Gaseous Flames,” Work-in-Progress Poster to be presented, 35th International Symposium on Combustion, San Francisco, CA, 3-8 August, 2014.
Y. Zhang, M. Kim, P.B. Sunderland, J.G. Quintiere, J. De Ris, D.P. Stocker, F. Takahashi, P.V. Ferkul, “Burning Rate Emulator for Microgravity Studies,” Work-in-Progress Poster to be presented, 35th International Symposium on Combustion, San Francisco, CA, 3-8 August, 2014.

Finally, an updated list of ACME Publications and Presentations is now available online.

ACME CONTACTS

 

Project Manager: J. Mark Hickman, NASA Glenn Research Center, 216-977-7105, john.m.hickman@nasa.gov

Deputy Project Manager: Andrew C. Suttles, NASA Glenn Research Center, 216-433-8328, andrew.c.suttles@nasa.gov

Project Scientist: Dennis Stocker, NASA Glenn Research Center, 216-433-2166, Dennis.P.Stocker@nasa.gov

Deputy Project Scientist: Dr. Fumiaki Takahashi, Case Western Reserve University, 216-433-3778, fumiaki.takahashi-1@nasa.gov

Engineering Team: ZIN Technologies, Inc.

ACME GALLERY