JPL Technical Report Server

The Mars Exploration Rovers entry descent and landing and the use of aerodynamic decelerators

The Mars Exploration Rovers entry descent and landing and the use of aerodynamic decelerators

Steltzner, A.; Desai, P.; Lee, W.; Bruno, R.
URI: http://hdl.handle.net/2014/7442
Date: 2003-05-20
Citation: Aerodynamic Decelerators Conference
Monterey, CA, USA

Abstract:

The Mars Exploration Rovers (MER) project, the next United States mission to the surface of Mars, uses extensive aerodynamic deceleration in during its entry, descent and landing (EDL) phase.

Show full item record

Items in TRS are protected by copyright, but are furnished with U.S. government purpose use rights.

Files in this item

Thumbnail
Name: 03-1306.pdf
Size: 2.923Mb
Format: PDF
View/Open

This item appears in the following Collection(s)

Search


Browse

My Account