Submarines and their Weapons - Aircraft of World War II
Submarines and their Weapons - Aircraft of World War II
Submarines and their Weapons - Aircraft of World War II
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SURFACE-TO-SURFACE MISSILES<br />
Above: An A4 rocket, shrouded in tarpaulin, on the railway<br />
flatcar used to transport it to the vicinity <strong>of</strong> the launch site.<br />
The Allied advance across northern Europe drove the V2<br />
battalions out <strong>of</strong> effective range <strong>of</strong> worthwhile targets.<br />
THE LATER GUIDED BALLISTIC MISSILE PROJECTS<br />
As soon as the A4 was viable, the project was taken<br />
out <strong>of</strong> von Braun's h<strong>and</strong>s. He <strong>and</strong> his team, it is suggested,<br />
were never entirely satisfied with it, <strong>and</strong><br />
would happily have gone on refining <strong>their</strong> design, but<br />
Heinrich Himmler, who had previously seized control<br />
<strong>of</strong> all the secret weapons programmes, would not<br />
accept that. Von Braun turned to working on ways <strong>of</strong><br />
increasing its range. The simplest means, he concluded,<br />
was to fit it with wings, so that it would glide in<br />
the final phase <strong>of</strong> its flight, prolonging its descent <strong>and</strong><br />
increasing its range to 435km (270 miles), but he<br />
counted without the effects <strong>of</strong> re-entering the dense<br />
air at lower atmospheric levels. The one A4b missile<br />
which was launched successfully (the first one<br />
crashed soon after take-<strong>of</strong>f) failed to re-enter cleanly<br />
<strong>and</strong> was destroyed.<br />
The A6, which never made it past the discussion<br />
stage, was to have been an A4 fueled by SV-StoiT,<br />
made up <strong>of</strong> 94 per cent nitric acid <strong>and</strong> 6 per cent<br />
nitrous oxide, <strong>and</strong> Visol (the generic name given to a<br />
group <strong>of</strong> isobutyl-vinyl esters); it was to have 20 per<br />
82<br />
cent more thrust. The A7 was a winged version <strong>of</strong> the<br />
A5, air-launched as a concept vehicle for the A9. The<br />
A8 was virtually identical to the A6 but fuelled with<br />
SV-St<strong>of</strong>f <strong>and</strong> diesel oil, although it is also suggested<br />
that it was to have been fuelled with LOX <strong>and</strong><br />
methanol contained in pressurized tanks, rather than<br />
employing the turbine pump to deliver them to the<br />
combustion chamber. The A9 was the A4b with modified<br />
wing planform: essentially, the horizontal fins<br />
were to have been continued forward, right to the<br />
rocket's nose, in a simple ogive, to allow it to survive<br />
re-entry; it had the motor from the A6, with a projected<br />
range <strong>of</strong> 600km (370 miles).<br />
The final ballistic missile project, the A10, was<br />
much more ambitious in scale <strong>and</strong> had it ever materialised,<br />
would have been the first ever ICBM. The projected<br />
inter-continental ballistic missile was to have<br />
been a two-stage rocket, the first stage being based on<br />
six A4 motors linked into a common venturi, <strong>and</strong><br />
designed to propel its second stage - either an A4 or<br />
an A9 - to an altitude <strong>of</strong> 24km (14.9 miles) before its<br />
own motor was fired, giving it a range <strong>of</strong> around<br />
4800km (2800 miles) with a 1000kg (22001b) amatol<br />
warhead <strong>and</strong> a flight time <strong>of</strong> around 45 minutes. It is<br />
suggested that this project was first discussed as early<br />
as 1940, long before the United States entered the<br />
war, but there is no evidence that it got beyond the