Theoretical performance of liquid ammonia and liquid fluorine as a rocket propellant Page: 4 of 23
This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided to Digital Library by the UNT Libraries Government Documents Department.
The following text was automatically extracted from the image on this page using optical character recognition software:
6 RESTRICTED NACA RM E53A26
Specific heat at constant pressure, cal/(g)(oK)
1 0 T( A
ep p T ' ni(C) + 2 nj() Yi " P ni( A()i7)
Derivative of logarithm of pressure with respect to logarithm of density
at constant entropy
2: p1 0
YS i (a)
. T s = p -( i ) A _N
Coefficient of viscosity, poise
S PM (9)
Coefficient of thermal coInductivity, cal/(s..ec)(cm)(oK)
k = 0 eg +4-M)(10)
Then co position is assumed to be frozen, equti.ons (7) and (8)
Sp.ecific heat at constant pressre assumi n g frozen composition
frozen Ln ora (1)
D .rv.... v .. o I0. 7itCt o2 pQesC:- t. th re.:A-4-ct. to logarIthn of density
ut c. m.. ut; , s c -i c.-f on cr -osition
(g -7M'2- /0 \
S ie ) l_ v frozen
09P" L.ozen M
Thy 1 as of vrice it exit well cond uctiviy for mixtures of
co tt-stion ga.-es calculated by ir, " of questions (9) and (i0) are only
Here’s what’s next.
This report can be searched. Note: Results may vary based on the legibility of text within the document.
Tools / Downloads
Get a copy of this page or view the extracted text.
Citing and Sharing
Basic information for referencing this web page. We also provide extended guidance on usage rights, references, copying or embedding.
Reference the current page of this Report.
Gordon, Sanford & Huff, Vearl N. Theoretical performance of liquid ammonia and liquid fluorine as a rocket propellant, report, July 3, 1953; (digital.library.unt.edu/ark:/67531/metadc53029/m1/4/: accessed November 15, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.