The crew and thermal systems division at JSC has developed an international space station (ISS) utilization payload for evaluating the carbon dioxide (CO2) control capability which utilizes a hamilton…

Ended Awarded

Contract number
NNJ12HE60D
Awardee
Awarding agency
Obligated
$20,711

Award facts

Contract value 100% obligated
$20,711.12 Current and potential, with all options
Completion date 100% complete
Current and potential, with all options
NAICS code
541330 Engineering Services
PSC
R425 Support- Professional: Engineering/Technical
Set-aside
No set-aside
Competition
Full and Open Competition · 1 offer Multiple Award, Fair Opportunity
Pricing
Firm Fixed Price
Place of performance
Windsor Locks, CT 06096, USA
Legislative mandates

Award details come from SAM.gov/FPDS.

Description

The crew and thermal systems division at JSC has developed an international space station (ISS) utilization payload for evaluating the carbon dioxide (CO2) control capability which utilizes a hamilton sundstrand developed carbon dioxide and moisture removal amine swing-bed (camras) in conjunction with water and air safe features in order to assess CO2 removal capability in a spaceflight environment. Hamilton sundstrand provided design and development support during the development phase of the payload. This included an initial feasibility assessment, requirements definition for the control and monitoring systems for the swingbed, and initial design of control and power handling modules for the payload. This payload is presently on orbit and, during initial operation, experienced an anomaly which requires the unique knowledge and skills of the hamilton sundstrand camras design team. This effort consists of evaluating swingbed payload fault tree analyses, identifying and supporting verification of potential root causes. The contractor s support will also be required to develop and evaluate recovery plans to ensure the proposed courses of action meet the intent specified. Troubleshooting efforts include concentrating on the valve stepper motor, interfacing electrical harnessing and motor control drive stage, however additional on-orbit troubleshooting may be necessary to yield further information to aid in diagnosis and remediation. Hamilton sundstrand, as the original developer of the amine swingbed, is necessary to support the investigation of payload failures as a part of a failure analysis group as potential causes are ruled out. Hamilton sundstrand has proprietary rights to a technology that is the baseline CO2 humidity removal technology for several future space vehicles. CO2 and humidity control technology is essential to the safe operation of a space craft. The camras was developed by hamilton sundstrand and has been under test in various configurations at NASA s johnson space center since 2006. Their historical knowledge of developing this technology is crucial to this effort.

Quick answers

Who was awarded contract NNJ12HE60D?

NNJ12HE60D was awarded to Hamilton Sundstrand Space Systems International, Inc. by Johnson Space Center (National Aeronautics and Space Administration) on August 23, 2012.

How much is contract NNJ12HE60D worth?

The government has obligated $20,711 on NNJ12HE60D.

Is contract NNJ12HE60D an order under another contract?

Yes. NNJ12HE60D is a delivery order under GS10F0439X, a federal supply schedule, on The Professional Services Schedule (PSS).

Was contract NNJ12HE60D competed?

The extent of competition for NNJ12HE60D was full and open competition. The government received 1 offer.

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