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Development of a Hermetically Sealed Canister for Sample Return Missions

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX16CP15C
Agency Tracking Number: 154580
Amount: $749,870.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: S4.05
Solicitation Number: N/A
Timeline
Solicitation Year: 2015
Award Year: 2016
Award Start Date (Proposal Award Date): 2016-04-27
Award End Date (Contract End Date): 2018-04-26
Small Business Information
Building 3, Suite 1005 63 Flushing Avenue Unit 150, Brooklyn, NY, 11205-1070
DUNS: 131364820
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Kris Zacny
 Principal Investigator
 (510) 207-4555
 zacny@honeybeerobotics.com
Business Contact
 Chris Chapman
Title: Chief Financial Officer
Phone: (646) 459-7809
Email: chapman@honeybeerobotics.com
Research Institution
N/A
Abstract
The goal of this project is to develop hermetic sealing technologies which can be used for the return of samples from planetary bodies such as Mars, the Moon, Comets and Asteroids, with a primary focus on induction brazing as a means of sealing a Mars Sample Return Orbiting Sample (OS) after it has been recovered by the MSR Orbiter spacecraft. During Phase 1, Honeybee Robotics investigated several techniques for providing hermetic sealing such as Knife Edge, Shape Memory Alloy, C-ring, O-ring and Induction Brazing. These were identified as promising hermetic sealing approaches which can be applied to Sample Return (SR) missions, such as the Flagship Mars SR, New Frontiers (NF) Comet SR and the Lunar South Pole-Aitken Basin SR, identified by the NRC Decadal Survey as the primary missions for the next decade. The sealing system would be used to store samples of rocks, soils, atmospheric gas, ice or icy-soil. Based on Phase 1, we determined that a brazing approach is the optimum method of sealing planetary samples and should be used as a primary seal. Knife edges and O-rings should be pursued as secondary and redundant (backup) seals, respectively. Therefore, we propose to design and fabricate hermetic sealing canisters and test their hermeticity to achieve leak rates of 10-7 atm cc/sec He. The canisters will be exposed to dust and thermal cycles to reach TRL 5/6 at the end of the Phase 2.

* Information listed above is at the time of submission. *

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