On the basis of the preliminary Scout trajectory plan, a launch window is defined for the revised X4 mission, which uses an Algol III Scout to inject the satellite into a nominally circular orbit at a height of 750 km. The effects of launch vehicle injection errors are taken into account using a stochastic simulation method.
Launch Window for the X4 Satellite on a Scout Rocket
1972
22 pages
Report
Keine Angabe
Englisch
AIAA | 1994
|Online Contents | 1994
|The Scout Launch Vehicle program
NTRS | 1981
|Scout S-200C Launch/Navy Transat
NTIS | 1977
NTIS | 1976