ACE spacecraft

被引：57

作者：

Chiu, MC ^{[1
]}

Von-Mehlem, UI ^{[1
]}

Willey, CE ^{[1
]}

Betenbaugh, TM ^{[1
]}

Maynard, JJ ^{[1
]}

Krein, JA ^{[1
]}

Conde, RF ^{[1
]}

Gray, WT ^{[1
]}

Hunt, JW ^{[1
]}

Mosher, LE ^{[1
]}

McCullough, MG ^{[1
]}

Panneton, PE ^{[1
]}

Staiger, JP ^{[1
]}

Rodberg, EH ^{[1
]}

机构：

[1] Johns Hopkins Univ, Appl Phys Lab, Laurel, MD 20707 USA

来源：

SPACE SCIENCE REVIEWS | 1998年 / 86卷 / 1-4期

关键词：

Deep Space Network; Power Subsystem; Propulsion Subsystem; Spacecraft Component; Solar Isotope Spectrometer;

D O I：

10.1023/A:1005002013459

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

The Johns Hopkins University Applied Physics Laboratory (JHU/APL) was responsible for the design and fabrication of the ACE spacecraft to accommodate the ACE Mission requirements and for the integration, test, and launch support for the entire ACE Observatory. The primary ACE Mission includes a significant number of science instruments - nine - whose diverse requirements had to be factored into the overall spacecraft bus design. Secondary missions for monitoring space weather and measuring launch vibration environments were also accommodated within the spacecraft design. Substantial coordination and cooperation were required between the spacecraft and instrument engineers, and all requirements were met. Overall, the spacecraft was kept as simple as possible in meeting requirements to achieve a highly reliable and low-cost design.

引用

页码：257 / 284

页数：28