<DOC>
<DOCNO>
1102
</DOCNO>
<TITLE>
a five-stage solid fuel sounding rocket system .
</TITLE>
<AUTHOR>
swanson, a.g.
</AUTHOR>
<BIBLIO>
nasa memo 3-6-59 l, 1959 .
</BIBLIO>
<TEXT>
a five-stage solid-fuel sounding-rocket system which can boost a payload
 of 25 pounds to an altitude of 525 nautical miles and that of 100
pounds to 300 nautical miles is described . data obtained from a typical
 flight test of the system are discussed .
</TEXT>
</DOC>
