NASA-LLIS-0424
Lessons Learned – Voyager Unbalanced Attitude Control System and Thruster Impingement Effects on Navigation (~1977)
contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
date accessioned | 2017-09-04T18:47:04Z | |
date available | 2017-09-04T18:47:04Z | |
date copyright | 07/10/1996 | |
date issued | 1996 | |
identifier other | KLBEQCAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std;query=autho162/handle/yse/228258 | |
description abstract | Abstract: Shortly after the launch of Voyager, unexpected dynamic effects necessitated additional orbit determination analysis, testing, and modeling to ensure an accurate trajectory. Perform careful coordinated pre-flight analysis to determine the impact of such effects as torques induced by solar pressure and gas impingement on the spacecraft structure. Design and test to avoid impingement problems. | |
language | English | |
title | NASA-LLIS-0424 | num |
title | Lessons Learned – Voyager Unbalanced Attitude Control System and Thruster Impingement Effects on Navigation (~1977) | en |
type | standard | |
page | 2 | |
status | Active | |
tree | NASA - National Aeronautics and Space Administration (NASA):;1996 | |
contenttype | fulltext | |
subject keywords | Hardware | |
subject keywords | Spacecraft | |
subject keywords | Trajectory Accuracy |