As already reported, Hayabusa carried two reaction wheels were lost on July 31st and October 3rd, and its attitude has been maintained by a single wheel together with the chemical engines aboard, while the spacecraft has been operated normally.

In order that the flight can be carried out and completed until the return to the Earth, the fuel consumption required for stabilizing the attitude has to be reduced, and a strenuous effort has been poured to devise the strategy including a number of firing tests in vacuum on the ground.

A new control scheme making the firing impulse enough small has now been developed assuring the attitude control resolution to be well managed. This assures the fuel amount required is adequate within that remains.

The on-orbit function test was already conducted and it was verified functioning by the actual flight hardware and software aboard. The Hayabusa project team concluded the flight operation until the return to the Earth is feasibly performed, as long as the existing instruments and hardware aboard continue working normally as they are.

The proximity operation assumed in November next month consists of one Rehearsal Descent plus two Touching-downs for sampling. They are scheduled as follows:

• Rehearsal Descent November 4th,
• 1st Touching-down for sampling November 12th,
• 2nd Touching-down for sampling November 25th.

These events will occur around noon in Japan Standard Time in the midst of the operation period from Japan. There are several Rehearsal and Touching-down sites candidates and the events instances may be shifted earlier or later by 6 hours at maximum, depending on the operation status. The concrete schedule will be released as soon as they are determined.

Hayabusa Succeeds In Observing The 'Oposition Surge' Of Itokawa Tokyo, Japan (SPX) Oct 28, 2005 How much brighter is the full Moon than the quarter Moon? If we consider the ratio of the illuminated area, "Double" seems to be a reasonable answer. But in reality, the full Moon is more than four times bighter than the quarter Moon. Why?

The "phase angle" is defined as the angle between the lines connecting tne Sun-Target and the Target-Observer. Namely, the phase angle for the quarter Moon is 90 degree, and that for the full Moon is almost 0 degree. It is well known that airless bodies in our Solar System, such as the Moon, generally show a brightness enhancement when the phase angle approaches zero. This phenenomenon is called the "opposition surge".

Do we observe the "opposition surge" on Itokawa? You can find the answer in the images below. The phase angle was abour 35 degrees for the left image and less than 1 degree for the right image.

The Hayabusa camera team confirmed the "oposition surge" through careful inspection of these images. More detailed analysis provides important information on the surface state, such as the difference between bare rocks and sands.

The observation of the "opposition surge" was not a serendipity, but one result of an elaborate operation. Hayabusa had to come to the Sun-Itokawa line at the distance of 3 hundred million kilometers from the Earth. The position tolerance was approximately the size of Itokawa, namely a few hundred meters. The Hayabusa navigation team accomplished the feat by skillful guiding.

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