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Security in Space The Next Generation - UNIDIR

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130<br />

Guidel<strong>in</strong>e 1: Limit debris released dur<strong>in</strong>g normal operations<br />

<strong>Space</strong> systems should be designed not to release debris dur<strong>in</strong>g normal<br />

operations. If this is not feasible, the effect of any release of debris on the<br />

outer space environment should be m<strong>in</strong>imized.<br />

Dur<strong>in</strong>g the early decades of the space age, launch vehicle and spacecraft<br />

designers permitted the <strong>in</strong>tentional release of numerous mission-related<br />

objects <strong>in</strong>to Earth orbit, <strong>in</strong>clud<strong>in</strong>g, among other th<strong>in</strong>gs, sensor covers,<br />

separation mechanisms and deployment articles. Dedicated design efforts,<br />

prompted by the recognition of the threat posed by such objects, have<br />

proved effective <strong>in</strong> reduc<strong>in</strong>g this source of space debris.<br />

Guidel<strong>in</strong>e 2: M<strong>in</strong>imize the potential for break-ups<br />

dur<strong>in</strong>g operational phases<br />

<strong>Space</strong>craft and launch vehicle orbital stages should be designed to avoid<br />

failure modes which may lead to accidental break-ups. In cases where a<br />

condition lead<strong>in</strong>g to such a failure is detected, disposal and passivation<br />

measures should be planned and executed to avoid break-ups.<br />

Historically, some break-ups have been caused by space system<br />

malfunctions, such as catastrophic failures of propulsion and power systems.<br />

By <strong>in</strong>corporat<strong>in</strong>g potential break-up scenarios <strong>in</strong> failure mode analysis, the<br />

probability of these catastrophic events can be reduced.<br />

Guidel<strong>in</strong>e 3: Limit the probability of accidental collision <strong>in</strong> orbit<br />

In develop<strong>in</strong>g the design and mission profi le of spacecraft and launch vehicle<br />

stages, the probability of accidental collision with known objects dur<strong>in</strong>g the<br />

system’s launch phase and orbital lifetime should be estimated and limited.<br />

If available orbital data <strong>in</strong>dicate a potential collision, adjustment of the<br />

launch time or an on-orbit avoidance manoeuvre should be considered.<br />

Some accidental collisions have already been identifi ed. Numerous<br />

studies <strong>in</strong>dicate that, as the number and mass of space debris <strong>in</strong>crease, the<br />

primary source of new space debris is likely to be from collisions. Collision<br />

avoidance procedures have already been adopted by some Member States<br />

and <strong>in</strong>ternational organizations.

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