Novel Hybrid Propulsion System for Sample Return Missions
Award amount
$749,956Program and phase
SBIR · Phase IIAward year
2017Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- PARABILIS SPACE TECHNOLOGIES, INC.
- Proposal award date
- 2017-06-07
- Contract end date
- 2018-12-06
- UEI
- WEMFVUG9KFJ9
- Solicitation number
- Not reported
- Topic code
- S4.03
Research abstract
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- Green Propellant Rapid Orbital Mobility Bus
- Acoustic Fluid Management Device
- Acoustic Fluid Management Device
- Low Cost Hybrid Rocket Orbital Transfer Stage
- Rapid Propellant Loading System
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Advanced Ignition System for Hybrid Rockets for Sample Return Missions
- Novel Hybrid Propulsion System for Sample Return Missions
- Additively Manufactured Monolithic Catalyst Bed for Green Propellants
- Electric Pump Fed Propulsion for a Liquid Bipropellant Mars Ascent Vehicle
- Ignition Systems for Long-Term Storage and Multi-Start Capability
Research funding history
28 SBIR/STTR records share this UEI (2015–2025). Reported award amounts total $9,188,737. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: National Aeronautics and Space Administration, Department of Defense