secondary cells with lithium anodes and immobilized fused_salt
secondary cells with lithium anodes and immobilized fused_salt secondary cells with lithium anodes and immobilized fused_salt
64. RECENT CHEMISTRY OF THE OXYGEN FLUORIDES I. J. Solomon, A. J. Kacmarek, J. K. Raney, J. N. Keith IIT Research Institute, Chicago, Illinois Some of the recent chemistry of the oxygen fluorides will be,discussed. The reaction of OF, a?$ SO, has been studied by using 0 labeled starting materials and 0 NMR spectroscopy, and evidence for an OF transfer mechanism is presented. Similar experiments with 0" labeled SO, and O,F, have shown that the reactions of O,F, can be explained in terms of an OOF transfer. The generality of this reaction is shown in that CF,CF(OOF)CF, and CF,CF,CF,OOF are formed by the reaction of O,F, and CF,CF=CF,.
I 65. GAS GEHEPAT'OR PROPELTANTS E. S. Sutton, C. F:. Vriesen, and E. J. Pacano~?slrj I Thiokol Chenical Corporation Elkton Division Elkton, Xaryland I The properties of ammonium perchlorate have made it the oxidizer of choice for composite sclid propellants for the past 20 years. Its ability to produce propellant comFositions with high flane tenperatures and densities has made it extremely useal to the missile propulsion industry. Recently, it has become possible to convert this versatile oxidizer to another nissilc S;JS~UJ application, that of wdm gcs Generator propellats. I Werm gas Cenerztor propellants are required for driviw turbine-alternator I systems for electrical power generation, for actuating jet-controlled attitude control system, and for propellin(; torpedo propulsion units. Despite the advantages or' m.ioniun perchlorate, it has been difficult to utilize it in these applications, because of the inherently high flame temperature (b500° to 55OOOF) of propellants 'Jased on it. Because of the materials of construction used in warn gas cenerator systems, the flame temperatures of these propellants are limited to values in the region of 2200' to 2300OF. In propellant technology, rechction of flame temperature is most conveniently obtained by rcducix the oxidizer to el (G//F) ratio to a verj 1011 value, so that the conposition is extremely fie1 rich. In Figure 1 a plot is shown of flame temperature versus the weight percent of llH4Cl04 for a mixture of ammonium perchlorate ani 2 Q-pical low oxygen content, high fuel content polymeric hydrocarbon binder. Although aluminum powder is normally used as a fuel component in solid propellants, it has been omitted for two reasons: it increases flame temperature to still hi&er (and undesirzble) values, while producing solid A1203 particles as ul eyhaust component. For most gas generator systems, the presence of solid perticles in the coalrustion products is extremely undesirable because of the resultvlt clogging and erosion of the metallic portions of the system. I Emuination of Figure 1 shows that the gradual reduction of the IIHqClOq 1, content from 9q: to 7% reduces the flame temperature from 5000'F down to the , desired level of 22009, simply by greatly reducing the oxidation ratio of the ! system. Tne oxidation ratio decreases from 4.33 down to 1.15 for these two 9 compositions, vhere oxidation ratio is defined as: A) Oxidation Ratio = co Atoms CC Atoms + 3 Df Atoms Unfortunately, this reduction .results in undesirably hi& levels of solid carbon in the coxxistion products vhen. these are exhausted to the ztmosphere. %is can be seen in Table 1, where the level for the hi& fuel content binder is 6.455 solid crr2cn by weight. iJo carbon is found in the combustion chamber at 1000 psia, but eqmion of the gases to 14.7 psia results in copious quantities of >lack snolre . wo methods are'applicable to the solution of this problem. The first of these involves substitution o$ much higher-oir.gen content binders for the polymeric fuel. In Figure 1 and Table I the results of substituting highly oxygenated polyester .
- Page 13 and 14: 13. Macerals. Macerals from a singl
- Page 15 and 16: i 1 I Photochemistry. A fundamental
- Page 17 and 18: t P li. al ’ i ._ m LL
- Page 19 and 20: ' 19. PYROLYSIS OF COAL IN A MICROW
- Page 21 and 22: I 21. In the third stage, the gas e
- Page 23 and 24: .4 4 0 W 0 m .d m x .-( 0 x w M m s
- Page 25 and 26: ' 25. CONCLUSIONS The principal rea
- Page 28 and 29: ' .4 b s tract 28.
- Page 30 and 31: 30. the course of the experiment Ex
- Page 32 and 33: d (Sulfur] dt m i trogenj dt 32. E
- Page 34 and 35: 34. Table 1, Properties of Feed Mat
- Page 36 and 37: 0 0 0 m 0 VI b N 0 c, VI N 0 v, N h
- Page 38 and 39: - Literature Cited 38 1. Gordon, K
- Page 40 and 41: 40 z - B 30 w 6 20 yl w U 10 40. 10
- Page 42 and 43: Z 0 In 80 CK W > 6 60- 0 I- 40- Z W
- Page 44 and 45: 44. 2.0 I 1.2 - 0 2 1.0- 0.8 i TIME
- Page 46 and 47: - 2.81 1.NITROGEN 2. SULFUR 3. GASO
- Page 48 and 49: 48. The oil from the separator is v
- Page 50 and 51: . 50 . Table I . Properties of Pitc
- Page 52 and 53: 52. Coke yield A - - - - 0 800 900
- Page 54 and 55: FIGURE 8. 54. t 0.5 1 800 900 1,000
- Page 56 and 57: Introduction 56. FLUORODINITROETUNO
- Page 58 and 59: chloride extractant without other h
- Page 60 and 61: 60. identified (Reference 7) as the
- Page 62 and 63: 62. to FEFO -e quite high (80 to 85
- Page 66 and 67: polymers for the conventional fuel
- Page 68 and 69: 68. In summary, two general methods
- Page 70 and 71: 70. Table XI1 Differential Thermal
- Page 72 and 73: vapor Pressure (psia) Figure 4. Vap
- Page 74 and 75: C H -0-C-NHF, - 2 5 II 0 74. H 9304
- Page 76 and 77: 76. The infrared spectrum is descri
- Page 78 and 79: , 78. PREPARATION AND POLYMERIZATIO
- Page 80 and 81: . .- . - ..... . . I ,caving the re
- Page 82 and 83: If it ~ 3 ~ o~t 7 s Y'2t the therm1
- Page 84 and 85: Chlorine Fentafluaride T q D OC 252
- Page 86 and 87: , 86. Zeections of Cl30 and AsF5. M
- Page 88 and 89: aa . - The rrost difficult rctionel
- Page 90 and 91: 90. DENSITY, VISCOSITY AND SURFACE
- Page 92 and 93: 92. If it is assumed that the syste
- Page 94 and 95: 94. After condensation of oxidizer
- Page 96 and 97: Stirring Solenoid LHe 7. Cryostat 9
- Page 98 and 99: Introduction 98. RFACTIONS OF OxYcm
- Page 100 and 101: , Acknowledgement 100. This work wa
- Page 102 and 103: 102. volume and then by pumping to
- Page 104 and 105: 104. The x-ray powder pattern (Tabl
- Page 106 and 107: Irredie tion Time, mi&) 106. Table
- Page 108 and 109: I. Introduction 108. RE7IIEw OF ADV
- Page 110 and 111: 1.40 w F O/) 103-4O 'F 110. /H 0 21
- Page 112 and 113: !P, "c -- -2118.5 -195 -172 -16.1 .
64.<br />
RECENT CHEMISTRY OF THE OXYGEN FLUORIDES<br />
I. J. Solomon, A. J. Kacmarek, J. K. Raney, J. N. Keith<br />
IIT Research Institute, Chicago, Illinois<br />
Some of the recent chemistry of the oxygen fluorides will<br />
be,discussed. The reaction of OF, a?$ SO, has been studied by using<br />
0 labeled starting materials <strong>and</strong> 0 NMR spectroscopy, <strong>and</strong> evidence<br />
for an OF transfer mechanism is presented. Similar experiments <strong>with</strong><br />
0" labeled SO, <strong>and</strong> O,F, have shown that the reactions of O,F, can be<br />
explained in terms of an OOF transfer. The generality of this reaction<br />
is shown in that CF,CF(OOF)CF, <strong>and</strong> CF,CF,CF,OOF are formed by the<br />
reaction of O,F, <strong>and</strong> CF,CF=CF,.