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Related Concept Videos

Impact: Problem Solving01:26

Impact: Problem Solving

In an experiment conducted during a Mars mission, a rover propels a projectile with an initial velocity, and the projectile rebounds after colliding with the Martian surface. To ascertain the maximum height attained by the projectile after this collision, the known restitution coefficient and acceleration due to gravity are employed.
By designating the launch point as the origin and utilizing kinematic equations, the vertical component of the projectile's velocity at the point of impact is...
Projectile Motion: Example01:18

Projectile Motion: Example

The theory of projectile motion is very useful for players of several sports to improve their performance. For example, a javelin thrower needs to throw their javelin in such a way that it travels as far as possible. The javelin thrower takes a short run-up to increase the initial speed of the javelin. The range of a projectile is at its maximum at a 45° angle so javelin throwers try to angle their throw as close to 45° as possible.
When we speak of the range (R) of a projectile on level...

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Related Experiment Video

Updated: Jul 12, 2026

A Test Bed to Examine Helmet Fit and Retention and Biomechanical Measures of Head and Neck Injury in Simulated Impact
07:30

A Test Bed to Examine Helmet Fit and Retention and Biomechanical Measures of Head and Neck Injury in Simulated Impact

Published on: September 21, 2017

Apollo 12 lunar module impact: laboratory simulation and possible downrange ballistic effects.

H F Swift, T R McGetchin, D D Preonas

    Science (New York, N.Y.)
    |August 28, 1970
    PubMed
    Summary

    Plastic pellet impacts on sand targets mimicked Apollo 12 lunar module (LM) impacts, creating shallow craters. Debris reimpacted downrange, but this ballistic rain did not explain the anomalous seismic signal.

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    Last Updated: Jul 12, 2026

    A Test Bed to Examine Helmet Fit and Retention and Biomechanical Measures of Head and Neck Injury in Simulated Impact
    07:30

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    Published on: September 21, 2017

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    06:14

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    Published on: July 30, 2020

    Conducting Elevated Temperature Normal and Combined Pressure-Shear Plate Impact Experiments Via a Breech-end Sabot Heater System
    10:52

    Conducting Elevated Temperature Normal and Combined Pressure-Shear Plate Impact Experiments Via a Breech-end Sabot Heater System

    Published on: August 7, 2018

    Area of Science:

    • Planetary Science
    • Impact Cratering Dynamics
    • Seismology

    Background:

    • The Apollo 12 mission experienced an anomalous seismic signal upon lunar module (LM) impact.
    • Understanding impact dynamics is crucial for interpreting planetary surface features and seismic data.

    Purpose of the Study:

    • To simulate lunar module impact conditions using plastic pellets on sand targets.
    • To investigate crater formation and ejecta patterns.
    • To assess the contribution of ballistic rain to anomalous seismic signals.

    Main Methods:

    • Plastic pellets were launched at sand targets simulating Apollo 12 LM impact conditions (4° launch angle, 1.68 km/s velocity).
    • Craters formed were analyzed for morphology (shallow elliptical or doublet).
    • Ejecta patterns and downrange reimpacts were studied.

    Main Results:

    • Shallow elliptical or doublet craters were formed, resembling lunar craters.
    • Analysis indicated that LM debris and crater ejecta skipped and reimpacted far downrange.
    • The observed ballistic rain did not fully account for the anomalous seismic signal.

    Conclusions:

    • Impact experiments can replicate lunar cratering features.
    • Reimpacting debris (ballistic rain) is a consequence of such impacts.
    • The anomalous seismic signal from the Apollo 12 LM impact requires further explanation beyond ballistic rain.