(a) nitrous oxide: N,O(g) - N,(g) + 1/2 0,(9) AG° - |kJ/mol AH° - kJ/mol Spontaneity spontaneous nonspontaneous Thermicity endothermic exothermic Suitability suitable not suitable
(a) nitrous oxide: N,O(g) - N,(g) + 1/2 0,(9) AG° - |kJ/mol AH° - kJ/mol Spontaneity spontaneous nonspontaneous Thermicity endothermic exothermic Suitability suitable not suitable
Chemistry
10th Edition
ISBN:9781305957404
Author:Steven S. Zumdahl, Susan A. Zumdahl, Donald J. DeCoste
Publisher:Steven S. Zumdahl, Susan A. Zumdahl, Donald J. DeCoste
Chapter1: Chemical Foundations
Section: Chapter Questions
Problem 1RQ: Define and explain the differences between the following terms. a. law and theory b. theory and...
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Among other things, an ideal fuel for the control thrusters of a space vehicle
should decompose in a spontaneous exothermic reaction when exposed to an
appropriate catalyst. Evaluate the following substances under standard state
conditions as suitable candidates for fuels. (Provide AG° and AH° in kJ/mol
reactant.)
(a) nitrous oxide:
N,0(g) → N2(9) + 1/2 0,(9)
AG° =
kJ/mol
AH° =
kJ/mol
Spontaneity
O spontaneous
O nonspontaneous
Thermicity
O endothermic
O exothermic
Suitability
O suitable
O not suitable
(b) diborane:
B,H,(9) - 2 B(s) + 3 H,(9)
AG° =
kJ/mol
AH° =
kJ/mol
Spontaneity
O spontaneous
O nonspontaneous
Thermicity
O endothermic
exothermic
Suitability
O suitable
O not suitable
(c) dinitrogen trioxide:
N,0,(9) – N,(9) + 3/2 0,(9)
AG° =
KJ/mol
AH° -
kJ/mol
Spontaneity
O spontaneous
O nonspontaneous
Thermicity
O endothermic
O exothermic
Suitability
O suitable
O not suitable
(d) aluminum hydride:
AIH, (s) – Al(s) + 3/2 H,(9)
AG° =
kJ/mol
ΔΗ' -
kJ/mol
Spontaneity
O spontaneous
O nonspontaneous
Thermicity
O endothermic
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