[meteorite-list] (Meteorite-list) Value of NEAR Shoemaker landing attempt
From: Sam Kimpton <bessel_at_meteoritecentral.com>
Date: Thu Apr 22 09:41:07 2004 Message-ID: <3A81BF09.D77090D3_at_europa.com> I do not believe the Spacecraft will rebound of the surface of 433 Eros. There are problems which will most likely impact (pardon the pun) the survivability of the landing. One problem is the spacecraft's velocity. Provided that the fuel supply is sufficient for the sustained that is planned the NEAR Shoemaker spacecraft is estimated to touch down at a velocity between 5 and 7 MPH. Add to this the unknown nature of the exact touch-down point and the lack of landing gear and one is faced with a pronounced likelyhood that the spacecraft will roll on contact and assume an unfavorable attitude for relaying data from the asteroid's surface. This whole thing was not part of the origional flight plan. It was more of an afterthought. The mission objectives have been met. NEAR Shoemaker functioned nominally in all respects and returned more data than origionally anticipated. The descent to the surface provides a good opportunity to develop and test software routines and procedures for approach and landing during future mining and impact mitigation missions to asteroids. Even if the "landing" or "docking" is a failure it will only be so in a partial sense. The experience will be of great value and will provide much need information for the next attempt on some other body. In addition the spacecraft will be integrating and sending images every thirty seconds during the four hour descent and will provide graphic data pertaining to 433 Eros' surface. Essentially this is a higher tech rendition of what was accomplished with the Ranger Missions to the Moon. The problem of planning the "landing" approach is much simpler in that 433 Eros has a single axis of rotation. Can you imagine what this would be like in the event that it became necesary to land on an object like Castalia which has a non principal one? The operation will not be carried on NASA TV owing to the attention given by it to the Shuttle mission. It will be carried on a seperate satelite. however I do not have the details. I will be watching none-the-less with great interest. As for the questions regarding seemingly anomolous surface processes on 433 Eros such as fracturing of rocks and boulders, flat units of crater infill, and mass wasting, could impact and radiative transport of the regolith be the causative factor? Food for thought. Sam Kimpton Director/Scientific Officer: Vernonia Peak Observatory http://www.nwag.portland.or.us/ http://www.nwastronomygroup.org Personal page: http://www.europa.com/~bessel/Impact/Impact.html Received on Wed 07 Feb 2001 04:32:57 PM PST |
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