Skip Navigation
SBIR/STTR

Titan Balloon Convection Model, Phase I

Completed Technology Project

Project Introduction

Titan Balloon Convection Model, Phase I
This innovative research effort is directed at determining, quantitatively, the convective heat transfer coefficients applicable to a Montgolfiere balloon operating in an atmosphere simulating that of Titan. It is anticipated that a platform such as this will provide the mobility desired to explore that part of the solar system. Utilizing only the waste heat available from an on board power source, it should be possible to circumnavigate Saturn's largest moon. Accurate knowledge of free convection is essential for predicting the performance and mitigating the risk for such a mission. In order to simulate a volume of gas large enough to inflate a model balloon at 77K, vacuum insulation panels will be used to minimize the thermal losses. At the conclusion of this Phase I effort, a final report will establish the feasibility of this approach and describe the future applications of this technology. More »

Primary U.S. Work Locations and Key Partners

Project Library

Share this Project

Organizational Responsibility

Project Management

Project Duration

Light bulb

Suggest an Edit

Recommend changes and additions to this project record.

This is a historic project that was completed before the creation of TechPort on October 1, 2012. Available data has been included. This record may contain less data than currently active projects.

^