I have a few questions about the Redstone and the Jupiter/Juno follow-ons:1. The Redstone test missiles seem to have had two different versions. One that had a tapered aft unit and warhead section and one that didn't. I am willing to admit that this might be a trick of photography that makes them look different, But it sure seems like there were two versions. See the photos below.2. It is my understanding that the Redstone missile, Jupiter-A, Mercury Redstone LVs, and the Sparta used the LOX/Alcohol fuel and the Jupiter-C and the Juno I used the LOX/Hydyne. Is this correct?3. Does anyone have a good photograph of the Jupiter-C reentry vehicle configuration as it sat on the LV prior to launch? There are very few photos of the 2nd and 3rd Jupiter-C vehicles so it is hard to tell how the warhead and adaptor were configured.Thank you!
I have a few questions about the Redstone and the Jupiter/Juno follow-ons:1. The Redstone test missiles seem to have had two different versions. One that had a tapered aft unit and warhead section and one that didn't. I am willing to admit that this might be a trick of photography that makes them look different, But it sure seems like there were two versions. See the photos below.
2. It is my understanding that the Redstone missile, Jupiter-A, Mercury Redstone LVs, and the Sparta used the LOX/Alcohol fuel and the Jupiter-C and the Juno I used the LOX/Hydyne. Is this correct?
3. Does anyone have a good photograph of the Jupiter-C reentry vehicle configuration as it sat on the LV prior to launch? There are very few photos of the 2nd and 3rd Jupiter-C vehicles so it is hard to tell how the warhead and adaptor were configured.