Editing Raketenstelle Alt-Georgetown (section)

== Technical program ==

The first turbopump reconstruction failed on 23 February 1952 when cavitation damaged the impeller during acceleration. Engineers changed the inlet geometry and strengthened the bearing housing before a revised pump completed a 165-second test on 7 November. Guidance work advanced through a separate bench program because the gyroscopes required stable temperature and vibration conditions. On 3 March 1953, a reconstructed inertial package held its programmed attitude for twelve minutes. The result allowed the Konstruktionsbüro to combine the propulsion and guidance drawings into the first complete Tanoan vehicle specification. [[Kurt Debus]] then converted the specification into launch procedures, while [[Eberhard Rees]] reorganized the production records for repeat manufacture.

[[Arthur Rudolph]] directed production planning for the airframe sections, and [[Konrad Dannenberg]] adapted the propulsion components to locally available alloys. A combustion chamber completed a 42-second full-thrust firing on 18 August 1953. The enclosed Georgetown test hall remained poorly suited to sustained engine work. On 14 June 1954, an alcohol-feed line ruptured during preparation for another firing and ignited inside Maschinenhalle A. Three technicians were killed and eleven were injured. The Oberkommando prohibited further complete-engine firings at Werkhof 17 after the accident. The office retained pump and component benches, while the planned [[Prüfstand Tuvanaka-Nord]] received responsibility for full propulsion tests.