Ariane 5 upper-stage ignition conditions improvement, and return to operation with "envisat" payload

被引:4
|
作者
Dutheil, JP [1 ]
Langel, G
机构
[1] Astrium GmbH, Space Infrastruct Div, Senior Expert Upper Stage, D-28361 Bremen, Germany
[2] Astrium GmbH, Space Infrastruct Div, Head Prop Div, D-81663 Munich, Germany
关键词
D O I
10.1016/S0094-5765(03)80020-6
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
ARIANE 5 experienced a flight anomaly with the 10(th) model mission (F 510), having placed its both satellites in a lower orbit than the planned GTO. Only one satellite (Artemis) could be retrieved due to its own propulsion systems. Arianespace, CNES and Astrium-GmbH (former DaimlerChrysler Aerospace Dasa) immediately set up a recovery team, combining forces for carrying deep and schedule-driven investigations, and later qualifying recovery measures. A failure in such an important program is immediately triggering a large "post-shock" reaction from the ARIANE community implied in the relevant business and technology. The investigation fields are summarised in the following chapters, showing how failure analysis, engineering investigations and basic research have been combined in order to have a schedule and methodic efficient approach. The combination of all available European resources in space vehicle design has been implemented, involving industry, agency technical centers and research laboratories. The investigation methodology applied has been driven by the particular situation of a flight anomaly investigation, which has to take into account the reduced amount of measurement available in flight and the necessary combination with ground test data for building a strategy to reach identification of possible failure scenario. Agency, dedicated to earth and climate monitoring, on flight 511, the 28/02/2002, from Kourou Spaceport. (C) 2003 International Astronautical Federation. Published by Elsevier Science Ltd. All rights reserved. From the investigations and from extensive sensitivity characterisation test of EPS engine (AESTUS) ignition transient, stability margins have been deeply investigated and introduced in the post-anomaly upgraded stage design The identification and implementation of recovery measures, extended as well to potential ignition margin reduction factors even beyond the observed flight anomaly allowed to establish a robust complementary qualification status, thus allowing resuming of operational flight, starting with the valuable "Envisat" payload of European Space Agency, dedicated to earth and climate monitoring, on flight 511, the 28/02/2002, from Kourou Spaceport. (C) 2003 International Astronautical Federation. Published by Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:585 / 595
页数:11
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