Spacecraft control main parachute inflation using reefing systems
Spacecraft and aerospace recovery systems utilize reefing systems, such as conventional reefing lines or staged inflation mechanisms, to control main parachute inflation and mitigate excessive deceleration forces.
The claim is a specific, verifiable technical fact about aerospace engineering. Retrieved papers explicitly discuss reefing lines and staging (e.g., twice-inflation and second reefing stages) used in parachute inflation control to regulate opening loads. Therefore, the claim is supported.
J. Redmond, G. Parker, T. Hinnerichs. Optimal load limiting parachute inflation control. 1995. https://doi.org/10.1017/S0001924000028487
This paper explicitly discusses conventional reefing lines and adaptive structures used to control parachute inflation and limit peak deceleration loads during deployment.
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Xiaojun Xing, Fenghao Li, Xiaoran Chen, Yilin Xun, Yiming Guo, Qi Wei. Research on the inflation process of the drag parachute in the landing of first-stage booster and its key parameters. 2020. https://doi.org/10.1109/CCDC49329.2020.9163957
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