Tesla TI2000GPU-24 User Manual

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the ground power support requirements are presented. Wherever practi-

cal, data is presented conservatively. However, NO GENERAL CONSERVATISM

HAS BEEN APPLIED. All performance data presented is within the appli-

cable limits of the Turbo Start.

5-1

SECTION II

DATA CRITERIA

5-3 DATA BASIS

The type of data used is indicated at the bottom of each performance

chart under DATA BASIS. The applicable report and date of the data

are also given. The data provided generally are based on one of

three categories:

Derived From Actual Controlled Testing.

Controlled test data

obtained on a similar unit type.

Calculated Data.

Data based on tests, but not on a similar

unit type placed under a controlled test.

Estimated Data

. Data based on estimates using rules of phys-

ics, mathematics, and electrical engineering principles and con-

cepts, but not verified by tests.

5-4. SPECIFIC CONDITIONS

The data presented are accurate only for specific conditions listed

under the title of each chart or graph. Variables for which data are

not presented, but which may affect that phase of performance, are

discussed in associated text. Where data are available or reasonable

estimates can be made, the amount that each variable affects perfor-

mance will be given.

5-5. GENERAL CONDITIONS

In addition to the specific conditions, the following general condi-

tions are applicable to the performance data.

Variation in Aircraft.

Power demand differences between indi-

vidual aircraft of the same make and model are known to exist due

to variations in DC electrical system efficiency. These differ-

ences, however, are considered insignificant and are not individu-

ally accounted for.

Ground Support and Aircraft Instrument Variations.

The data