Five different formulations of a rocket propellant x1 may be used in an aircrew escape systems on the observed burning rate Y. Here, each of the formulation is prepared by mixing from a batch of raw materials x2 which can support only five formulations required for the purpose of testing.
Usage
data(rocket)
Format
A data frame with 25 observations on the following 4 variables.
y
burning rate
batch
raw materials batch
op
experience of the operator
treat
formulation type of the propellant ABCDE
References
Montgomery, D. C. (1976-2012). Design and Analysis of Experiments, 8e. J.Wiley.
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> library(ACSWR)
> png(filename="/home/ddbj/snapshot/RGM3/R_CC/result/ACSWR/rocket.Rd_%03d_medium.png", width=480, height=480)
> ### Name: rocket
> ### Title: Rocket Propellant
> ### Aliases: rocket
> ### Keywords: latin square design
>
> ### ** Examples
>
> data(rocket)
> matrix(rocket$treat,nrow=5)
[,1] [,2] [,3] [,4] [,5]
[1,] "A" "B" "C" "D" "E"
[2,] "B" "C" "D" "E" "A"
[3,] "C" "D" "E" "A" "B"
[4,] "D" "E" "A" "B" "C"
[5,] "E" "A" "B" "C" "D"
> par(mfrow=c(1,3))
> plot(y~factor(op)+factor(batch)+treat,rocket)
> rocket_aov <- aov(y~factor(op)+factor(batch)+treat,rocket)
>
>
>
>
>
> dev.off()
null device
1
>