Engineering Model Atmosphere of Mars.
Purchase Print Copy
|Add to Cart||Paperback17 pages||$15.00||$12.00 20% Web Discount|
A technical model of the Martian atmosphere that gives extreme upper and lower probable limits between which must fall the atmospheric parameters of pressure, temperature, and density up to 150-km altitude over middle and low latitudes. Other parameters important to the engineering design of entry probes are tabulated. The results have a rather high confidence value. Although the values are extremely widespread, a combination of circumstances indicates that the engineering task of atmospheric entry will be easier for Mars than for any other planet. 17 pp.
This report is part of the RAND Corporation Paper series. The paper was a product of the RAND Corporation from 1948 to 2003 that captured speeches, memorials, and derivative research, usually prepared on authors' own time and meant to be the scholarly or scientific contribution of individual authors to their professional fields. Papers were less formal than reports and did not require rigorous peer review.
This document and trademark(s) contained herein are protected by law. This representation of RAND intellectual property is provided for noncommercial use only. Unauthorized posting of this publication online is prohibited; linking directly to this product page is encouraged. Permission is required from RAND to reproduce, or reuse in another form, any of its research documents for commercial purposes. For information on reprint and reuse permissions, please visit www.rand.org/pubs/permissions.
The RAND Corporation is a nonprofit institution that helps improve policy and decisionmaking through research and analysis. RAND's publications do not necessarily reflect the opinions of its research clients and sponsors.