MIL-HDBK-1003/7
Table 8
Theoretical Steam Rates
LB/KWH
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* Pin,PSIG
1600 *
100
200
250
400
600
850
1250
1450
* Tin,F
1000 *
Sat.
Sat.
550
750
825
900
950
1000
*
*
*
*
* 1" HGA
10.20
9.17 8.09
6.85
6.34
5.92
5.62
5.43
5.40
* 2" HGA
*
11.31 10.02 8.78
7.36
6.76
6.28
5.94
5.73
5.69
* 3" HGA
*
12.12 10.62 9.27
7.71
7.05
6.53
6.16
5.93
5.89
*
* 0 PSIG
22.73 17.52 14.57 11.19
9.82
8.81
8.10
7.72
7.62
* 5 PSIG
*
26.07 19.35 15.90 11.99 10.42
9.29
8.49
8.07
7.96
*
* 10 PSIG
29.52 21.10 17.15 12.71 10.96
9.71
8.83
8.38
8.26
* 15 PSIG
*
33.20 22.83 18.35 13.38 11.44 10.08
9.14
8.66
8.52
* 20 PSIG
*
37.17 24.56 19.53 14.02 11.90 10.43
9.42
8.91
8.76
*
* 25 PSIG
41.56 26.31 20.70 14.63 12.34 10.76
9.68
9.14
8.98
* 50 PSIG
*
74.8 35.99 26.75 17.56 14.31 12.22 10.80 10.15
9.94
*100 PSIG
*
66.6 42.40 23.86 18.07 14.77 12.65 11.78 11.46
*
*150 PSIG
71.8 31.93 22.15 17.33 14.35 13.26 12.79
*200 PSIG
*
43.51 26.96 20.05 16.05 14.72 14.08
*300 PSIG
*
40.65 26.53 19.66 17.74 16.70
*
*400 PSIG
78.3 35.43 23.82 21.10 19.52
*500 PSIG
*
49.03 28.87 25.03 22.69
*600 PSIG
*
73.1 35.30 29.79 26.35
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The equation for the theoretical steam rate is as follows:
EQUATION:
T.S.R. = 3413/(h1 - h2)
(1)
where:
T.S.R. = theoretical steam rate of the turbine, lb/kWh
h1 = throttle enthalpy at the throttle pressure and
temperature, Btu/lb
h2 = extraction or exhaust enthalpy at the exhaust pressure
based on isentropic expansion, Btu/1b.
5.1.8.2
efficiency and includes the entire performance and mechanical and electrical losses of
the turbine and generator. The engine efficiency can be calculated using the following
equation:
EQUATION:
ne =
(h1 - he)ntng/(h1 - h2)
(2)
56