A Saturn V with stretched S-IC and S-II stages with four US-1207 solid rocket boosters.
Nov 112013
Nov 102013
A Saturn S-II stage as a first stage with an S-IVB second stage, with four UA-1207 solid rocket boosters.
Nov 092013
A Saturn S-II stage as a first stage with an S-IVB second stage, with four UA-1205 solid rocket boosters.
Nov 082013
A Saturn Ib with four UA-1205 solid rocket boosters with thrust vector control.
Nov 072013
A Saturn Ib with a stretched S-IB first stage and two UA-1207 solid rocket boosters.
Nov 062013
A Saturn Ib with a stretched S-IB first stage and four UA-1207 solid rocket boosters.
Nov 052013
A Saturn Ib with a stretched S-IB first stage and four UA-1205 solid rocket boosters.
Nov 042013
A Saturn Ib with four UA-1205 solid rocket boosters.
Nov 032013
United Tech produced some spiffy propaganda/PR back in the day. One thing I have is a surprisingly large book on the UA-1205/1207 solid rocket motor, used on the Titan IIIC. At the back of it is some very 1960’s artwork of proposed uses of the solid motors on variants of the Saturn I and Saturn V. 
Oct 292013
Artwork of a three-stage rocket designed by Krafft Ehricke around 1953. 126 feet tall, it would be capable of orbiting 11,000 pounds of payload into a 600 mile circular orbit. Liftoff weight would be 1.3 million pounds.
The first stage, here being shown dropped, would be parachute recovered. the second stage would be expended; the third stage would be used to built up a space station. If you can’t immediately tell where stage 2 ends and stage 3 begins, it’s because stage 3 is the central cylinder, with stage 2 being wrapped around it. This sort of staging arrangement was considered fairly often in the days before they actually had to build these things.
It would be able to land 3,000 pounds on the moon or shoot 5,000 pound probes past Mars or Venus.
