Structural, thermal, and optical performance (STOP) modeling and results for the James Webb Space Telescope integrated science instrument module

被引：9

作者：

Gracey, Renee ^{[1
]}

Bartoszyk, Andrew ^{[2
]}

Cofie, Emmanuel ^{[3
]}

Comber, Brian ^{[4
]}

Hartig, George ^{[5
]}

Howard, Joseph ^{[2
]}

Sabatke, Derek ^{[1
]}

Wenzel, Greg ^{[6
]}

Ohl, Raymond ^{[2
]}

机构：

[1] Ball Aerosp, 1600 Commerce St, Boulder, CO 80301 USA

[2] NASA, Goddard Space Flight Ctr, Greenbelt Rd, Greenbelt, MD 20771 USA

[3] SGT Inc, 7515 Mission Dr,Suite 300, Seabrook, MD 20706 USA

[4] Comber Thermal Solut, 8367 Silver Trumpet Dr, Columbia, MD 21045 USA

[5] Space Telescope Sci Inst, 3700 San Martin Dr, Baltimore, MD 21218 USA

[6] Sierra Lobo Inc, 6301 Ivy Lane,Suite 620, Greenbelt, MD 20770 USA

来源：

MODELING, SYSTEMS ENGINEERING, AND PROJECT MANAGEMENT FOR ASTRONOMY VII | 2016年 / 9911卷

关键词：

STOP; ISIM; structural; thermal; optical; gravity; jitter;

D O I：

10.1117/12.2233641

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

The James Webb Space Telescope includes the Integrated Science Instrument Module (ISIM) element that contains four science instruments (SI) including a Guider. We performed extensive structural, thermal, and optical performance (STOP) modeling in support of all phases of ISIM development. In this paper, we focus on modeling and results associated with test and verification. ISIM's test program is bound by ground environments, mostly notably the lg and test chamber thermal environments. This paper describes STOP modeling used to predict ISIM system performance in 0g and at various on-orbit temperature environments. The predictions are used to project results obtained during testing to on-orbit performance.

引用

页数：20

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