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Rose Propulsion Lab

Rose Propulsion Lab is a Rose-Hulman Institute of Technology student team developing liquid bipropellant propulsion systems for a propulsive lander challenge. Rose-Hulman sources document subscale engine development, systems and component work toward a 550-lbf engine, and a student hot-fire liquid-rocket-engine test; this record makes no orbital or flight-success claim.

Identity

Field
Liquid bipropellant rocket engines, propulsion systems, subscale engine development, hot-fire testing, propulsive landers, and systems integration
Name
Rose Propulsion Lab
Region
NA
Status
active

Details

Description
Rose Propulsion Lab is a Rose-Hulman Institute of Technology student team developing liquid bipropellant propulsion systems for a propulsive lander challenge. Rose-Hulman sources document subscale engine development, systems and component work toward a 550-lbf engine, and a student hot-fire liquid-rocket-engine test; this record makes no orbital or flight-success claim.
Latitude
39.4829201
Location
Longitude
-87.3241582
University

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Creation Time
August 14, 2026 at 05:50:34 UTC
Updated Time
August 14, 2026 at 05:50:34 UTC