Aerocapture Technology Developments by the In-Space Propulsion Technology Program

Show full item record

Please use this identifier to cite or link to this item:

Title: Aerocapture Technology Developments by the In-Space Propulsion Technology Program
Author: Munk, Michelle Marie
Abstract: This paper will explain the investment strategy, the role of detailed systems analysis, and the hardware and modeling developments that have resulted from the past 5 years of work under NASA's In-Space Propulsion Technology (ISPT) Program, Aerocapture investment area. The organizations that have been funded by ISPT over that time period received awards from a 2002 NASA Research Announcement. They are: Lockheed Martin Space Systems, Applied Research Associates, Inc., Ball Aerospace, NASA's Ames Research Center, and NASA's Langley Research Center. Their accomplishments include improved understanding of entry aerothermal environments, particularly at Titan, demonstration of aerocapture guidance algorithm robustness at multiple bodies, manufacture and test of a 2-meter Carbon-Carbon "hot structure," development and test of evolutionary, high-temperature structural systems with efficient ablative materials, and development of aerothermal sensors that will fly on the Mars Science Laboratory in 2009. Many of NASA's current programs are benefitting from the sustained ISPT support for Aerocapture, component technologies are mature enough to be infused on entry missions, and the aerocapture system technology is ready to be validated in flight.
Description: This presentation was part of the session : Cross Cutting Technologies Sixth International Planetary Probe Workshop
Type: Proceedings
Date: 2008-06-26
Contributor: United States. National Aeronautics and Space Administration
Langley Research Center
Relation: IPPW08. Cross Cutting Technologies
Publisher: Georgia Institute of Technology
Subject: Aerocapture
Technology development
Ablative materials
Aerothermal modeling

All materials in SMARTech are protected under U.S. Copyright Law and all rights are reserved, unless otherwise specifically indicated on or in the materials.

Files in this item

Files Size Format View Description
23-261-1-PB.pdf 40.74Kb PDF View/ Open PDF Abstract

This item appears in the following Collection(s)

Show full item record