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当前航天飞机与挑战者号发射前飞行服在发射加速过程中的伸展能力比较。

Comparison of current Shuttle and pre-Challenger flight suit reach capability during launch accelerations.

作者信息

Bagian J P, Schafer L E

机构信息

Anthropometry and Biomechanics Lab, NASA-Johnson Space Center, Houston, TX.

出版信息

Aviat Space Environ Med. 1992 Jul;63(7):624-8.

PMID:1616441
Abstract

The Challenger accident prompted the creation of a crew escape system which replaced the former Launch Entry Helmet (LEH) ensemble with the current Launch Entry Suit (LES). However, questions were raised regarding the impact of this change on crew reach capability. Our study addressed the question of reach capability and its effect on realistic ground-based training for Space Shuttle missions. Eleven subjects performed reach sweeps in both the LEH and LES suits during 1 and 3 Gx acceleration trials in the Brooks AFB, TX, centrifuge. These reach sweeps were recorded on videotape and subsequently analyzed using a three-dimensional motion analysis system. The ANOVA procedure of the Statistical Analysis System (SAS) program was used to evaluate differences in forward and overhead reach. The results showed that the LES provided less reach capability than its predecessor, the LEH. This study also demonstrated that, since there was no substantial difference between 1 and 3 Gx reach sweeps in the LES, realistic Shuttle launch training may be accomplished in ground-based simulators.

摘要

“挑战者”号事故促使了乘员逃逸系统的创建,该系统用当前的发射进入服(LES)取代了原来的发射进入头盔(LEH)套装。然而,有人对这一变化对乘员伸展能力的影响提出了疑问。我们的研究探讨了伸展能力的问题及其对航天飞机任务实际地面训练的影响。11名受试者在德克萨斯州布鲁克斯空军基地的离心机中进行1Gx和3Gx加速度试验时,分别穿着LEH和LES套装进行了伸展扫描。这些伸展扫描被录制在录像带上,随后使用三维运动分析系统进行分析。使用统计分析系统(SAS)程序的方差分析程序来评估向前和向上伸展的差异。结果表明,LES的伸展能力比其前身LEH要小。这项研究还表明,由于LES在1Gx和3Gx伸展扫描之间没有实质性差异,实际的航天飞机发射训练可以在地面模拟器中完成。

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