IGF::OT::IGF AN ON-BOARD OXYGEN CONCENTRATOR IS REQUIRED DURING LONG DURATION MANNED SPACE MISSIONS TO SUPP…
Award details are derived from public USAspending.gov records. Not a bid recommendation.
Award details
- Award ID
- NNX14CC55P
- Contractor
- Awarding agency
- National Aeronautics and Space Administration
- Sub-agency / office
- National Aeronautics and Space Administration
- Award amount
- $0
- Period of performance
- Jun 20, 2014 – Dec 19, 2014
- NAICS
- 541712 — Research and Development in the Physical, Engineering, and Life Sciences
- PSC
- PSC AR11
- Place of performance
- CO
Public award description
IGF::OT::IGF AN ON-BOARD OXYGEN CONCENTRATOR IS REQUIRED DURING LONG DURATION MANNED SPACE MISSIONS TO SUPPLY MEDICAL OXYGEN. THE COMMERCIAL MEDICAL OXYGEN GENERATORS BASED ON PRESSURE SWING ADSORPTION (PSA) ARE LARGE AND HIGHLY POWER INTENSIVE. TDA RESEARCH, INC. (TDA) PROPOSES TO DEVELOP A SMALL, LIGHTWEIGHT, PORTABLE OXYGEN GENERATOR BASED ON A VACUUM SWING ADSORPTION (VSA) TO PRODUCE CONCENTRATED MEDICAL OXYGEN. THE UNIT USES AMBIENT VEHICLE CABIN AIR AS THE FEED AND DELIVERS HIGH PURITY OXYGEN WHILE MEETING NASA'S REQUIREMENTS FOR HIGH FLOW CAPACITY, CLOSED-LOOP TISSUE OXYGEN CONTROL AND OPERATION IN MICROGRAVITY/PARTIAL GRAVITY. TDA'S VSA SYSTEM USES A MODIFIED VERSION OF THE LITHIUM EXCHANGED LOW SILICA X ZEOLITE (LI-LSX), A STATE-OF-THE-ART AIR SEPARATION SORBENT EXTENSIVELY USED IN COMMERCIAL PORTABLE OXYGEN CONCENTRATORS (POCS) TO ENHANCE THE N2 ADSORPTION CAPACITY. IN PHASE I, WE WILL DEMONSTRATE THE SCIENTIFIC, TECHNICAL, AND COMMERCIAL FEASIBILITY OF THE OXYGEN CONCENTRATOR MODULE (OCM). THE CONCENTRATOR WILL HAVE AN ADJUSTABLE PRESSURE OUTPUT TO PRODUCE 2-15 LPM OF O2 AT 50 PERCENT TO MORE THAN 90 PERCENT PURITY FROM AMBIENT CABIN AIR. THE OCM WILL BE CAPABLE OF SELF-REGULATING THE OXYGENATION OF THE PATIENT USING A CLOSED LOOP FEEDBACK SYSTEM THAT SENSES TISSUE OXYGENATION LEVEL. WE WILL EVALUATE THE SORBENT PERFORMANCE IN A BREADBOARD BENCH-SCALE PROTOTYPE UNDER SIMULATED MICROGRAVITY/PARTIAL GRAVITY EXPLORATION ATMOSPHERES AND CARRY OUT A 10,000 CYCLE TEST (AT A MINIMUM) TO DETERMINE ITS LONG-TERM PERFORMANCE AND MECHANICAL DURABILITY. BASED ON THE EXPERIMENTAL RESULTS, WE WILL CARRY DESIGN THE DEMONSTRATION UNIT, OPTIMIZE ITS POWER DRAW OVER THE RANGE OF FLOWS AND OXYGEN LEVELS, AND DETERMINE ITS WEIGHT, VOLUME AND HEAT REJECTION REQUIREMENTS. THIS DESIGN WILL ALSO INCLUDE AN INLET FILTER DESIGNED TO REMOVE POTENTIAL SMOKE OR TOXIC GASES.
Find out who's winning similar federal contracts
Discover comparable awards, related contractors, and agency purchasing history.