Spacecraft Fire Detection and Suppression (FDS) Systems: An Overview and Recommendations for Future Flights 932166
As manned spacecraft have evolved into larger and more complex configurations, the mandate for preventing, detecting, and extinguishing on-board fires has grown proportionately to ensure the success of progressively ambitious missions. The closed environment and high value of manned spacecraft offer the Fire Detection and Suppression (FDS) systems designer significant challenges.
With the presence of Oxygen (O2), flammable materials, and ignition sources, it is impossible to completely remove the likelihood of a spacecraft fire. Manned spacecraft contain these three ingredients for fire; therefore, it becomes profitable to review past designs of FDS systems and ground testing to determine system performance and lessons learned in the past for present and future applications.
The objective of this paper is to present a brief summary of past FDS designs and to provide a discussion of suppressant agent options for future spacecraft utilizing available information and suppressant and detector test data in this field. A final recommendation for future spacecraft suppressant agent and fire detection methods, based upon this discussion, is the goal of this paper.
Citation: Martin, C. and DaLee, R., "Spacecraft Fire Detection and Suppression (FDS) Systems: An Overview and Recommendations for Future Flights," SAE Technical Paper 932166, 1993, https://doi.org/10.4271/932166. Download Citation
Author(s):
Charles E. Martin, Robert C. DaLee
Affiliated:
McDonnell Douglas Aerospace
Pages: 17
Event:
International Conference On Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Also in:
SAE 1993 Transactions: Journal of Aerospace-V102-1
Related Topics:
Fire detection
Hazardous materials
Spacecraft
Fire
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