High Performance Hybrid Upper Stage for NanoLaunch Vehicles, Phase I

Metadata Updated: March 23, 2019

Parabilis Space Technologies, Inc. (Parabilis), in collaboration with Utah State University (USU), proposes a low cost, high performance launch vehicle upper stage using oxygen and a novel additively manufactured polymer fuel grain as propellants in response to solicitation T1.01, Affordable Nano/Micro Launch Propulsion Stages. This technology will fulfill the ever-growing mission demands of the CubeSat and NanoSat market by enabling dedicated launch for 5-6 kg class payloads. Comparable launch vehicle stages in this size class are not currently commercially available. The proposed green-propellant system will have significant advancements over alternative technologies in cost, safety, and mission capability. During Phase I, the development team's objectives include preliminary design of an upper stage and the test fire of a demonstration prototype. This innovative stage is designed such that it can integrate directly into NASA Marshall's NanoLaunch 1200 architecture.

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Public: This dataset is intended for public access and use. License: U.S. Government Work

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Metadata Created Date August 1, 2018
Metadata Updated Date March 23, 2019

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Harvested from NASA Data.json

Additional Metadata

Resource Type Dataset
Metadata Created Date August 1, 2018
Metadata Updated Date March 23, 2019
Publisher Space Technology Mission Directorate
Unique Identifier TECHPORT_33483
Maintainer Email
Public Access Level public
Bureau Code 026:00
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Metadata Catalog ID https://data.nasa.gov/data.json
Schema Version https://project-open-data.cio.gov/v1.1/schema
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Harvest Source Id 39e4ad2a-47ca-4507-8258-852babd0fd99
Harvest Source Title NASA Data.json
Data First Published 2016-06-01
Homepage URL https://techport.nasa.gov/view/33483
License http://www.usa.gov/publicdomain/label/1.0/
Data Last Modified 2018-07-19
Program Code 026:027
Source Datajson Identifier True
Source Hash 62269ac217f276c556d46820549282294084c406
Source Schema Version 1.1

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