4.7 Article

Infiltration-controlled combustion of magnesium for power generation in space

Journal

COMBUSTION AND FLAME
Volume 238, Issue -, Pages -

Publisher

ELSEVIER SCIENCE INC
DOI: 10.1016/j.combustflame.2021.111950

Keywords

Combustion of metals; Combustion of powders; Infiltration; Magnesium; Space power systems

Funding

  1. Early Stage Innovations grant from NASA's Space Technology Research Grants Program [80NSSC20K0293]
  2. NASA Space TechnologyResearch Fellowship [80NSSC17K0161]

Ask authors/readers for more resources

Chemical heat integrated power systems offer high energy densities and long lifetimes, making them suitable for space missions. A study on a new concept of such a system combining a metal combustor and a chemical oxygen generator reveals the phenomena of propagation of a thermal wave and reverse ignition caused by infiltration-controlled combustion of metal powders. The experiment shows that coflow combustion can be achieved when a metal with a low Pilling-Bedworth ratio is used.
Chemical heat integrated power systems can potentially provide high energy densities and long lifetimes compared to the best batteries. They are of interest for space missions where the use of solar or nuclear energy is impractical. In a new concept of such a system, a metal combustor is coupled with a chemical oxygen generator, and the metal powder bed inside the combustor burns with the infiltrated oxygen. However, the infiltration-controlled combustion of metal powders is not well understood. In the present work, a magnesium powder poured in a vertical quartz tube was ignited by a laser inside a chamber filled with oxygen at pressures of 44 - 90 kPa. The ignition resulted in the propagation of a thermal wave followed by a second ignition at the other end and propagation of a thermal wave backward. Highspeed and infrared video recordings as well as thermocouple measurements were used for diagnostics. The results demonstrate that if a metal with a low Pilling-Bedworth ratio (0.81 for magnesium) is used, coflow combustion is possible. The coflow combustion wave propagates at incomplete conversion, with an axial velocity being as low as 0.1 mm/s and the zone of the highest temperature traveling along a helical path. An increase in the axial velocity of the combustion wave is accompanied by an increase in the flame thickness and a decrease in the extent of conversion. (c) 2021 The Combustion Institute. Published by Elsevier Inc. All rights reserved.

Authors

I am an author on this paper
Click your name to claim this paper and add it to your profile.

Reviews

Primary Rating

4.7
Not enough ratings

Secondary Ratings

Novelty
-
Significance
-
Scientific rigor
-
Rate this paper

Recommended

No Data Available
No Data Available