SBIR/STTR Research Award

Ultrahigh Energy Propulsion By Pulsed Magnetic Field Compression of Fissile Plas

Award identifier 4c3be370791aee612b6f7b2c0d6af4523d203eb98fcb30424b580f4a1a1ed5c6Awarding agency National Aeronautics and Space Administration

Award amount

$599,999

Program and phase

SBIR · Phase II

Award year

2002

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
New Era Technology
Proposal award date
Not reported
Contract end date
Not reported
UEI
JFDJUF42YFV3
Solicitation number
Not reported
Topic code
Not reported

Research abstract

A new fission powered space power and propulsion system based on using a non-moving fissile gas is proposed. The main innovation in the proposed fission based propulsion system is the use of well-established fusion plasma confinement and compression methods to achieve a supercritical condition in a highly subcritical fissile gas. In particular, electromagnetic induced shock wave compaction and gas dynamic trap techniques are merged to bring a relatively small volume ( 1 m3) of a fissile (235U, 233U, or 239Pu) compound gas (such as UF4) to prompt supercriticality condition, thereby, releasing an intense pulse of fission power. A magnetic field compaction scheme is designed to directly convert the fission energy to electricity. The specific energy of the proposed nuclear electric system for megawatt level power operation is well above 1 kWe/kg. An alternative direct propulsion system is designed based on using a merger between Magnetized Target Fusion (MTF) and hydrodynamic confinement techniques to achieve long duration ( 100 to 1000 ms) criticality and ultrahigh burnup in a fissile gas. The MTF technique induces a large pressure ratio ( 10) adiabatic compaction of fissile gas by rapid collapsing of a cylindrical layer of a low neutron absorbing metal (Al or Zr). Hydrodynamic confinement in a leaky reversed mirror configuration is used to contain and direct the fission plasma through a nozzle, thereby, generating intense thrust ( 100s of klb) at specific impulse levels in excess of 2000 seconds.

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.

Research funding history

11 SBIR/STTR records share this UEI (1995–2007). Reported award amounts total $3,309,566. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense

Agency intelligence

National Aeronautics and Space Administration

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