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用于航天器应用的干热灭菌建模。

Dry heat sterilization modelling for spacecraft applications.

作者信息

Flax Brian, Tortora Andrew, Yeung Yen, Schubert Wayne W, McDonnell Gerald

机构信息

Microbiological Quality & Sterility Assurance, Johnson & Johnson, Raritan, New Jersey, USA.

Biotechnology and Planetary Protection Group, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California, USA.

出版信息

J Appl Microbiol. 2022 Nov;133(5):2893-2901. doi: 10.1111/jam.15748. Epub 2022 Aug 5.

Abstract

AIMS

Inactivation processes using heat are widely used for disinfection and sterilization. Dry heat sterilization of spacecraft equipment has been the preferred microbial inactivation method as part of interplanetary travel protection strategies. An antimicrobial model, based on temperature and exposure time based on experimental data, was developed to provide reliable sterilization processes to be used for interplanetary applications.

METHODS AND RESULTS

Bacillus atrophaeus spores, traditionally used to challenge dry heat sterilization processes, were tested over a range of temperatures in comparison with spores of Bacillus canaveralius that have been shown to have a higher heat resistance profile. D-value and Z-values were determined and used to develop a mathematical model for parametric sterilization applications. The impact of the presence of a contaminating soil, representative of Mars dust, was also tested to verify the practical application of the model to reduce the risk of microbial contamination in such environments.

CONCLUSION

The sterilization model developed can be used as an intrinsic part of risk reduction strategies for interplanetary protection.

SIGNIFICANCE AND IMPACT

Forward and backward planetary protection strategies to reduce the risks of microbial contamination during interplanetary exploration and research is an important consideration. The development of a modern sterilization model, with consideration of microorganisms identified with higher levels of heat resistance than traditionally deployed in terrestrial applications, allows for the consideration of optimal inactivation processes to define minimum criteria for engineering design. The ability to inactivate living microorganisms, as well as to degrade biomolecules, provides a reliable method to reduce the risk of known and potentially unknown contaminants in future applications.

摘要

目的

利用热进行的灭活过程广泛用于消毒和灭菌。作为行星际旅行保护策略的一部分,对航天器设备进行干热灭菌一直是首选的微生物灭活方法。基于实验数据,开发了一种基于温度和暴露时间的抗菌模型,以提供用于行星际应用的可靠灭菌过程。

方法与结果

与已显示具有更高耐热性的卡纳维拉尔芽孢杆菌的孢子相比,对传统上用于挑战干热灭菌过程的萎缩芽孢杆菌孢子在一系列温度下进行了测试。确定了D值和Z值,并用于开发参数化灭菌应用的数学模型。还测试了代表火星尘埃的污染土壤的存在的影响,以验证该模型在降低此类环境中微生物污染风险方面的实际应用。

结论

所开发的灭菌模型可作为行星际保护风险降低策略的固有组成部分。

意义与影响

在行星际探索和研究期间减少微生物污染风险的向前和向后行星保护策略是一个重要考虑因素。开发一种现代灭菌模型,考虑到与传统上在地面应用中使用的微生物相比具有更高耐热性的微生物,有助于考虑最佳灭活过程以确定工程设计的最低标准。灭活活微生物以及降解生物分子的能力为降低未来应用中已知和潜在未知污染物的风险提供了一种可靠的方法。

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