Chapter 27 Questions Flashcards

1
Q

To achieve the same EIRP you can have high power with ________ TX antenna gain or low power with _____ antenna gain.

a. fixed, variable
b. dynamic, static
c. low, high
d. high,low

A

c. low, high

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2
Q

Doubling the distance between TX and RX would increase the space losses by ____ times.

a. 2
b. 8
c. 4
d. Space loss is independent of distance

A

c. 4

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3
Q

The comm link for a new science mission requires an Eb/No of 5 dB to achieve the required BER. If the EIRP is 1 dBW, Ls is -145 dB, La is -1 dB, Gr is 10 dB, the data rate is 60 dB, and the system noise temperature is 26 dB. What is the link margin?

a. 2.6 dB
b. 5 dB
c. 0 dB
d. 3 dB

A

a. 2.6 dB

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4
Q

Match the following steps in the Cost Estimating Process with the appropriate tasks.

Define the level and scope of the cost estimate.

a. Evaluation
b. Input.
c. Execution

A

b. Input

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5
Q

Match the following steps in the Cost Estimating Process with the appropriate tasks.

Apply cost adjustments.

a. Evaluation
b. Input.
c. Execution

A

c. Execution

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6
Q

Match the following steps in the Cost Estimating Process with the appropriate tasks.

Collect baseline mission information from design engineers; establish estimation ground rules.

a. Evaluation
b. Input.
c. Execution

A

b. Input

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7
Q

Match the following steps in the Cost Estimating Process with the appropriate tasks.

Determine major cost drivers for potential reductions

a. Evaluation
b. Input.
c. Execution

A

a. Evaluation

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8
Q

Match the following steps in the Cost Estimating Process with the appropriate tasks.

Assess the mission’s cost risk and calculate project or program reserves.

a. Evaluation
b. Input.
c. Execution

A

c. Execution

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9
Q

Match the following steps in the Cost Estimating Process with the appropriate tasks.

Test sensitivity of lifecycle costs to key assumptions and requirements.

a. Evaluation
b. Input.
c. Execution

A

a. Evaluation

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10
Q

Match the following Cost Estimating Methods discussed in this lesson with the statements that best fit.

Primary method used during Pre-Phase A and Phase A; when we know or can estimate only a few key variables.

a. Analogy
b. Parametric Cost Model
c. Grassroots

A

b. Parametric Cost Model

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11
Q

Match the following Cost Estimating Methods discussed in this lesson with the statements that best fit.

Also known as a “bottoms-up” estimate; requires a detailed design and understanding of the elements that constitute the system.

a. Analogy
b. Parametric Cost Model
c. Grassroots

A

c. Grassroots

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12
Q

Match the following Cost Estimating Methods discussed in this lesson with the statements that best fit.

Typically time-consuming; can’t typically prepare many of them during trade studies of advanced system concepts; primary method for Phases C and D.

a. Analogy
b. Parametric Cost Model
c. Grassroots

A

c. Grassroots

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13
Q

Match the following Cost Estimating Methods discussed in this lesson with the statements that best fit.

Most common example is a statistical Cost Estimating Relationship (CER) which uses a single equation or set of equations to relate one or more system characteristics to cost.

a. Analogy
b. Parametric Cost Model
c. Grassroots

A

b. Parametric Cost Model

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14
Q

Match the following Cost Estimating Methods discussed in this lesson with the statements that best fit.

A way to estimate cost based on a component having functional and performance characteristics similar to one whose cost is known.

a. Analogy
b. Parametric Cost Model
c. Grassroots

A

a. Analogy

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15
Q

Match the following Cost Estimating Methods discussed in this lesson with the statements that best fit.

Can be applied to any level of detail in a system; often proves to be unworkable and inflexible for trade studies.

a. Analogy
b. Parametric Cost Model
c. Grassroots

A

a. Analogy

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16
Q

Based on the 1988 cost comparison of crewed and robotic spacecraft performed by the NASA HQ Comptroller’s Office, crewed spacecraft have ___________ subsystems as robotic spacecraft. Design and development costs for crewed spacecraft hardware are ___________ for robotic spacecraft.

a. more than twice as many, about three times more than
b. the same number of, about four times more than
c. more than three times as many, about two times more than
d. the same number of, about the same

A

a. more than twice as many, about three times more than

17
Q

True/False: Two of the most common and traditional cost drivers include mass and quantity.

A

True