

Artemis II: The Translunar Injection Burn
Passage
•
Physics
•
9th - 12th Grade
•
Practice Problem
•
Easy
Mike Jones
Used 1+ times
FREE Resource
10 questions
Show all answers
1.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is the primary purpose of the Translunar Injection (TLI) burn?
To launch the Orion spacecraft from the surface of the Earth
To transition the spacecraft from Earth orbit to a path toward the Moon
To slow the spacecraft down for a landing on the lunar surface
To test the emergency escape systems of the European Service Module
2.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Which component of the Orion spacecraft is responsible for performing the TLI burn?
The Heat Shield
The Lunar Lander
The European Service Module (ESM)
The Solid Rocket Boosters
3.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
To what speed must Orion accelerate during the TLI burn to break free from Earth's orbit?
17,500 mph
Over 24,000 mph
50,000 mph
10,000 mph
4.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
How does the shape of Orion's orbit change after the TLI maneuver?
It changes from a square orbit to a circular orbit
It remains in a stable circular orbit
It changes from a circular orbit to an elliptical trajectory
It becomes a straight line directly to the Moon
5.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What is a "free-return trajectory"?
A path that allows the spacecraft to return to Earth naturally after looping the Moon
A mission path where the fuel is provided for free by international partners
A trajectory that requires constant engine firing to maintain
A maneuver used only in case of a total system failure during launch
6.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
Why is the TLI burn described as a "point of no easy return"?
The astronauts cannot breathe once the burn starts
The spacecraft is committed to the journey toward the Moon once it is completed
The engines are discarded immediately after the burn
The Earth's gravity completely stops pulling on the spacecraft
7.
MULTIPLE CHOICE QUESTION
30 sec • 1 pt
What could happen if the TLI burn is executed for too long?
The spacecraft would fall back to Earth immediately
The spacecraft could overshoot the Moon
The spacecraft would enter a permanent circular orbit around the Sun
The engines would freeze due to deep space temperatures
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