iampete wrote:
The decomposition of hydrazine is highly exothermic (per Wikipedia, combustion chamber temperatures hit ~800 C) and produces large volumes of hot gas. Would it not be reasonable to expect that exposure to the plumes even of a second or less (assuming the plumes are at least a meter or two in length just prior to touchdown) would have created some visible deformation/sculpting/whatever to the patches if they were in fact ice?
Pete, that is quite possible. You write the exhaust gasses are hot (1000K in the combustion chamber) and they have a large volume. I have to estimate the volume and its pressure. Well, estimate, it is rather a wild guess. Suppose 1 m³ of hot gas at 100 kPa pressure comes free during the last few seconds. Since the temperature is high, the mass of the exhaust is smaller than at 273K. Roughly four times smaller: 0.25 kg.
Specific heat of ice at 200 K is 1.5kJ/kg/K
Specific heat of nitrogen gas at 500 K is 1 kJ/kg/K.
Melting heat of ice: 240 kJ/kg
So solve the equation:
Cooling the hot gas - heating up and melting ice = 0, or:
0.25 * 1 * (1000-273) + x * ( 1.5 * (150-273) - 240) = 0. This leads to:
x = 0.25 * 737 / (240 + 185) = 0.45 kg
(mass * specific heat * temperature difference = heat)
Half a liter of water! Feasible, when one looks at the size of the holes in the soil.
It is better to flip the image upside down, it looks a bit more logical. My impression of the size of the holes: roughly 0.1m wide and 0.1m deep. However, there is no reference other than some pebbles near the hole.
Concluding: the amount of ice to melt is of an order of magnitude comparable to the potential size of the holes. It is neither 1000 larger nor 1000 times smaller. So melting can not be excluded, however it is not proven that the melting hypothesis is true. We need more accurate volumes and pressures of the exhaust gasses. Thats an item to be dealt with by NASA's rocket scientists.
About the 'barnacles':
iampete wrote:My gut feel is that that is unlikely. Thruster shutdown likely takes on the order of tens, possibly a few hundred, of milliseconds and the amount of non-decomposed hydrazine is probably miniscule as the thruster temperature still remains high.
It is more likely to be soil that was displaced by either the plumes and/or the shock of actual landing that, in falling back down, happened to stick to the structure.
You are right about the trusters. Shut those down immediatedly, if you want an undisturbed site! But why does this dust stick to the tubes? A rounded pebble lying on a round tube is in a very unstable position. To put this to the test, tilt a broomstick to the wall an drop randomly some pebbles on the broomstick. Do they stick on the broomstick? You may try a meter of rain drain pipe as well.
Moreover there are some protruding objects at the side of the tube. Those should have been falling down. These object can not be seen on the other legs, most likely due to the limited resolution of the jpg and its lossy compression. I hope to stumble over a lossless image, like TIFF or png. Maybe something for an APOD in the near future?
Note: I had to edit this message due to a silly error. Where i had
heat capacity written, it should have been
specific heat. That has been corrected now.