Question 1
Which statement best describes the topology of MIL-STD-1553?
Correct Answer:
MIL-STD-1553 is a dual-redundant, multi-drop bus supporting multiple remote terminals.
Explanation:
MIL-STD-1553 uses a wired, shared medium where a single Bus Controller can address many Remote Terminals on the same bus. It is designed as dual-redundant, meaning there are two independent conductor paths so the system keeps working even if one path has a fault. This setup is multi-drop, allowing multiple RT devices to be connected to the same bus and operated under a command/response scheme. The bus isn’t a single wire, isn’t wireless, and isn’t limited to one point-to-point link; instead, it relies on a shared, redundant two-wire pair that several devices can connect to and communicate over in a coordinated, time-multiplexed fashion.
Question 2
What causes the night effect?
Correct Answer:
The changing height of the ionosphere causing it to reflect skywaves.
Explanation:
The night effect comes from the ionosphere changing its properties when solar radiation drops. During the day the D layer is present and absorbs lower HF signals, limiting how far they can skip. At night the D layer fades away, reducing that absorption, and the main reflecting layer (the F layer) also shifts in height. This change in height and density means skywaves are refracted back to Earth from higher altitudes, increasing the distance over which they can travel and be received. In short, the ionosphere’s height and reflective behavior change with the day–night cycle, enabling longer-range skywave propagation.
Question 3
Which voltage powers the ADF antenna drive motor?
Correct Answer:
115VAC
Explanation:
Aircraft electrical systems for avionics typically provide 115 VAC at 400 Hz to power motors and components. This high-frequency AC makes the power transformers lighter and the motors simpler and more compact, which is why the ADF antenna drive motor is designed to run from that source. The other options don’t fit the usual avionics power scheme: 28 VDC is used for some DC buses but the ADF drive is an AC motor, 26 VAC isn’t a standard aircraft supply, and 230 VAC isn’t the common avionics standard in this context. So the motor is powered by 115 VAC to match the aircraft’s normal avionics power distribution.
Question 4
In TACAN operation, which data are provided in transmit-receive mode?
Correct Answer:
Range, Bearing, and Station Identification
Explanation:
TACAN in transmit-receive mode is designed to give a complete navigation picture: you get range, bearing, and the station’s identification. The range comes from the DME-like two-way exchange—the interrogator and transponder timing provide the distance to the station. The bearing comes from the TACAN’s azimuth information, telling you the direction to the station. The station identification is continuously broadcast so you can confirm which TACAN site you’re tracking. Together, these three data items—distance, direction, and ID—are why this mode provides the full set of TACAN information.
Question 5
What does triple-modular redundancy (TMR) consist of, and how does it affect reliability?
Correct Answer:
Three identical processing paths with a majority vote to determine the output, masking up to two simultaneous faults
Explanation:
Triple-modular redundancy uses three identical processing paths running in parallel and a majority vote to determine the final output. The idea is that if one path develops a fault and starts producing a wrong result, the other two paths will still agree on the correct result, so the voter selects the correct output and the fault is masked. This setup greatly boosts reliability because you only need two of the three paths to be correct for the system to behave correctly, reducing the impact of a single component failure. To give a sense of the improvement, if each path has reliability R, the chance that the majority output is correct is R^3 + 3R^2(1−R). That yields a substantial increase over a single path, especially when R is already high (for example, with R about 0.99, the overall reliability becomes around 0.9997). However, remember this protection is against a single faulty path; two simultaneous faults can still defeat the majority decision, and the voter itself is an extra component that can fail.
Question 1
Exam overview

About this Exam

Prepare with the ATO Mission Computers Practice Test practice quiz. This question bank includes 10 questions covering describes, effect, radalt, mission, and computers. Use it to review important concepts, identify knowledge gaps, and build confidence for the related exam, course, or assessment.

More details

Additional Information

ATO Mission Computers Practice Test

This practice set contains 10 questions from the matching question bank and focuses on describes, effect, radalt, mission, and computers. Work through each question carefully, review the provided solutions, and revisit topics that need more study before your next attempt.

This is an independent study resource intended for practice and review; it is not an official examination or an endorsement by any organization named in the title.

Quiz information

Frequently Asked Questions

The complete question count is available after full access is unlocked.
No fixed duration is currently configured for this quiz.
Question explanations are included where they are available in the quiz content, helping you review the reasoning after answering.
Yes. You can retake the practice test again as you continue studying during your available access period.
After your access is confirmed, you can continue into the complete practice exam from this quiz flow.
Unless explicitly stated otherwise, this page provides independent practice material for study and exam preparation and is not the official examination itself.
Keep studying

Related Questions