IP Library Granted Patent US 9,149,795
Granted Patent B2
US 9,149,795 · App. 13/115,814 · Granted Oct 6, 2015

Corrosion resistant catalysts for decomposition of liquid monopropellants

Inventors: Ender Savrun (Seattle, WA); Stephanie J. Sawhill (Bothell, WA)
Assignee: Sienna Technologies, Inc.
B01J21/066B01J23/40B01J23/468B01J35/002B01J37/0018B01J37/0036B01J37/0201B01J37/32F02C3/14F02K9/70F02K9/80
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Quick Facts
Patent No.
US 9,149,795
App. No.
13/115,814
Granted
Oct 6, 2015
Kind
B2
Abstract

Ceramic catalyst carriers that are mechanically, thermally and chemically stable in a ionic salt monopropellant decomposition environment and high temperature catalysts for decomposition of liquid high-energy-density monopropellants are disclosed. The ceramic catalyst carrier has excellent thermal shock resistance, good compatibility with the active metal coating and metal coating deposition processes, melting point above 1800° C., chemical resistance to steam, nitrogen oxides and acids, resistance to sintering to prevent void formation, and the absence of phase transition associated with volumetric changes at temperatures up to and beyond 1800° C.

Claims (18)

1. A stabilized ceramic catalyst comprising:

a ceramic selected from the group consisting of zirconia (ZrO 2 ), hafnia (HfO 2 ), and a mixture thereof;

at least one stabilizer selected from the group consisting of In 2 O 3 , SnO 2 , Ga 2 O 3 , and Sb 2 O 3 ;

a catalytically active metal; and

wherein the ceramic is formed as a plurality of particles and housed within a catalyst bed for a rocket engine.

2. A stabilized ceramic catalyst comprising:

a ceramic selected from the group consisting of zirconia (ZrO 2 ), hafnia (HfO 2 ), and a mixture thereof;

at least one stabilizer selected from the group consisting of In 2 O 3 , SnO 2 , Ga 2 O 3 , and Sb 2 O 3 ;

a catalytically active metal; and

wherein the ceramic is formed as a plurality of particles and housed within a thrust chamber for a rocket engine.

3. A stabilized ceramic catalyst comprising:

a ceramic selected from the group consisting of zirconia (ZrO 2 ), hafnia (HfO 2 ), and a mixture thereof;

at least one stabilizer selected from the group consisting of In 2 O 3 , SnO 2 , Ga 2 O 3 , and Sb 2 O 3 ;

a catalytically active metal; and

wherein the ceramic is formed as a plurality of particles and housed within a catalyst bed or a thrust chamber for a rocket engine, the ceramic further comprising at least one second stabilizer, the second stabilizer comprising one or more of MgO, Y 2 O 3 , CaO, or a lanthanide.

4. The stabilized ceramic catalyst of claim 3 wherein the catalytically active metal comprises at least one metal selected from the group consisting of platinum, rhodium, ruthenium, rhenium, osmium, iridium, iridium/rhodium alloy, and iridium/osmium alloy.

5. The stabilized ceramic catalyst of claim 3 wherein the catalytically active metal is dispersed on the surface of the plurality of stabilized ceramic particles.

6. The stabilized ceramic catalyst of claim 3 , wherein the ceramic is formed from a mixture of zirconia and hafnia.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 25, 2011
From: SAVRUN, ENDER; SAWHILL, STEPHANIE J.
To: SIENNA TECHNOLOGIES, INC.
Reel/Frame 026338/0947 →
Continuity (1)
Related Publication 20120297779A1 · Nov 29, 2012