NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
High-Temperature Systems Capability Summary NASA has been developing technology and systems for use on future missions, such as potential Venus landers, under projects such as LLISSE and HOTTech. A small (`15kg-50kg, depending on lifetime and science payload) Venus lander / entry shell system concept was developed as a potential ride along to a Venus orbiter. The simple deployment approach is for the carrier/orbiter spacecraft to point the lander/shell combination and release it for autonomous entry. Deceleration and touchdown of the lander is accomplished just as done by Soviet landers several times in the past.
Document ID
20250004648
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Tibor Kremic
(Glenn Research Center Cleveland, United States)
Date Acquired
May 7, 2025
Subject Category
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: Mission Formulation Planning Meeting
Location: Virtual
Country: US
Start Date: May 16, 2025
Sponsors: European Space Agency (ESA)
Funding Number(s)
WBS: 811073
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
LLISSE
long-duration
lander
high-temperature
Venus
No Preview Available