THIXOTROPIC IRFNA GEL
Assignee
US Government
Filed as: UNITED STATES OF AMERICA, AS REPRESENTED BY THE SECRETARY OF THE ARMY
Filed
May 26, 1983
Granted
Dec 26, 2000
Location
Huntsville AL (NASA/Army)
Abstract
A thixotropic oxidizer gel comprising inhibited red fuming nitric acid (IRFNA) as the carrier with lithium nitrate (LiNO3) suspended therein and gelled with a gellant agent of SiO2 having a mean particle size of 0.015 microns has the rheological properties which can be tailored to match those of MICOM GEL, a fuel gel. A thixotropic gelled fuel (MICOM GEL) has been of particular interest because of its increased safety, reduced sloshing, ease of pumping at zero gravity and ability to suspend high concentrations of high-energy ingredients. However, a gelled oxidizer has been desired for use with the gelled fuel to constitute a thixotropic gelled propellant system. The combination of a gelled fuel (MICOM GEL) and a gelled oxidizer is now a reality after the development of the thixotropic oxidizer gel disclosed above. Of major significance is the matching of the rheologial properties of the two gels so that an oxidizer/fuel (O/F) ratio shift does not occur with a temperature change. The development of the thixotropic oxidizer gel obviates the problems of O/F shift attributed to using a liquid IRFNA oxidizer with MICOM GEL. The combination of the thixotropic oxidizer gel comprising the carrier of IRFNA in weight percent amounts from about 55.0 to 86.0, the suspended LiNO3 in weight percent amounts from about 10.0 to 40.0, and the gellant agent of SiO2 in weight percent amounts from about 4.0 to about 5.0 with MICOM GEL fuel offers both high Isp and high density Isp which translates to significant increases in total system performance. This combination reflects a range increase to 160 percent of the present system.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jan 3, 1984
Rescinded
Aug 16, 2000
Duration
16 years, 7 months
Inventor
- 1BARRY D. ALLAN
Sensitive facility: Huntsville AL (NASA/Army)
Record Details
- Patent number
- US 6165293
- Application
- 06500642
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
US GovernmentMore from this assignee
ROTATING SHUTTER FOR EYE/OPTICS PROTECTION AGAINST IN-BAND FREQUENCY AGILE LASERS
US Government
COMPACT HIGH-ENERGY AUXILIARY POWER METHOD AND MEANS
US Government
THERMALLY MASSIVE RADAR DECOY
US Government
ADAPTIVE STEERABLE NULL ANTENNA PROCESSOR WITH NULL INDICATOR
US Government
INCREASING BURNING RATE OF SOLID PROPELLANTS BY ELECTRIC FIELD EFFECTS
US Government
MEASUREMENT OF JAMMING EFFECTIVENESS BY CROSS CORRELATION TECHNIQUES(C)
US Government
Related by domain
INERTIAL NAVIGATION ACCURACY ENHANCEMENT
BRITISH AEROSPACE PUBLIC LIMITED COMPANY
METHOD OF FORMING TEXTURED HIGH-TEMPERATURE SUPERCONDUCTORS
INTEGRATED CIRCUIT METALLIZATION WITH SUPERCONDUCTOR BEOL WIRING
TOSHIBA CORP.
FIXED INTERVAL BACKGROUND AUTO-ALIGNMENT FOR CLOSED LOOP INTERFEROMETRIC FIBER OPTIC GYROSCOPES
AAI CORPORATION
METHOD FOR MAKING HIGH-CRITICAL-CURRENT-DENSITY YBA2CU307 SUPERCONDUCTING LAYERS ON METALLIC SUBSTRATES
LOCKHEED MARTIN ENERGY RESEARCH CORPORATION
SUPERCONDUCTING CURRENT LEAD
JAPAN ATOMIC ENERGY RESEARCH INSTITUTE; FUJI ELECTRIC CO., LTD.; SUMITOMO ELECTRIC INDUSTRIES, LTD.