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document title / titre du document TRP W ORK PLAN ... - emits - ESA

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<strong>TRP</strong> Work Plan 2005-2007<br />

Description of Activities<br />

TEC-SB/7935/dc<br />

12/Feb/09<br />

<strong>TRP</strong> Reference:<br />

Title:<br />

T603-38EC<br />

Enhanced CCD Star Tracker<br />

Since the intro<strong>du</strong>ction of the Autonomous Star Trackers in the 1990s, their popularity and use on space missions has steadily<br />

increased until today were these units are used on all classes of mission and are becoming the sensor of choice for almost all<br />

missions.<br />

The European space in<strong>du</strong>stry has been at the forefront of this technology development, indeed in 2000/2001 there were<br />

nearly 15 European companies developing or selling star trackers. This amount of competition was unsustainable and so, at a<br />

harmonisation meeting in 2001, it was decided to no longer support the development of CCD based star trackers and<br />

concentrate instead on targeted developments to pro<strong>du</strong>ce the next generation of star trackers based on APS detectors, these<br />

having the potential to allow lighter, more compact and cheaper Star Trackers that simultaneously offered higher robustness.<br />

In<strong>du</strong>stry was left to support itself for the CCD star trackers. This policy had the desired effect of re<strong>du</strong>cing the number of<br />

European Star Tracker manufacturers dramatically while simultaneously forcing manufacturers to improve their units and<br />

re<strong>du</strong>ce prices. Today there are 5 star tracker suppliers in Europe, each of whom have survived by being highly competitive on<br />

the world stage. With a manageable number of suppliers, a large proportion of each of these companies business now coming<br />

from outside Europe and there still being an expected overlap of 2 to 4 years between CCD based and APS based star<br />

tracker supply it is now time to resume providing support to maintain and improve the existing CCD based pro<strong>du</strong>ct lines.<br />

The Terma HE-5AS STR has been selected for Cryosat, Aeolus and the LPF missions. Following the loss of Cryosat at launch<br />

it is also expected to fly on Cryosat 2. Work performed now to secure the STR and improve its robustness, reliability and<br />

qualification status will therefore have a near term beneficial effect on several <strong>ESA</strong> missions.<br />

This policy was clearly expressed in <strong>ESA</strong>/IPC(2005)70 rev.1, calling for pro<strong>du</strong>ct improvements of CCD Star Tracker , mainly<br />

for recurring platforms. According to the outcomes of the 2005 Harmonisation Roadmap on AOCS Sensors and Actuators, the<br />

present activity aims at: ensuring the availability of the HE-5AS to <strong>ESA</strong> projects for at least the next 3 years; improving the<br />

robustness and ease of use of the HE-5AS within the scope of the existing electrical design limitations; improving the<br />

straylight and thermal design and the understanding of their interactions and dependencies on the s/c system and orbital<br />

environment. This will result in the following main three tasks: 1. Software improvements for Robustness and Reliability; 2.<br />

Component obsolescence and Europeanisation; 3. System level analysis and improvements. This measure is implemented in<br />

line with IPC(2005)30, rev. 1 (Formal review of the geographical distribution of contracts), calling for a DG's additional effort to<br />

improve the geographical return of certain countries, including Denmark.<br />

Deliverables:<br />

In-flight data analysis report; design improvements and trade off report; improved SW design report; SW Test<br />

plan/proce<strong>du</strong>res/report<br />

Current TRL:<br />

TRL3-4 Target TRL: Application Need/Date: TRL8 (in-flight demo on<br />

TRL5-6<br />

Cryosat-2) by 2009<br />

Application/Mission: All missions Contract Duration: 18 months<br />

T-25, T26, T-27, T-29, T-30,<br />

SW Clause : - Dossier0 Ref.:<br />

T-33, T-34, T-965<br />

Consistency with Harmonisation<br />

Conclusions: <strong>ESA</strong>/IPC(2005)70 rev.1<br />

Roadmap and Conclusions:<br />

Page 156 of 227

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