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He112 R

1,303 18348627996  5.3 years ago
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Auto Credit Based on 18348627996's He112 B-0

[SADAMB][From other magacine]Early experiments with rocket propulsion EditIn 1931, the Army Weapons Office testing ground at Kummersdorf had taken over research into liquid-fuel rockets. In 1932, Wernher von Braun designed a rocket of this kind which used high percentage spirit and liquid oxygen. With this he made the first experiments. In 1934 he fired his second rocket type, the A2, from the North Sea island of Borkum. Having completed the programme of experiments, von Braun was interested in evaluating an aircraft with a rocket motor propulsion system. For this he needed an aircraft and support team. Initially the highest levels at the Army High Command and the Reich Air Ministry (RLM) were opposed to such "fantasies", as they called them. Many people, technicians and academic experts in positions of influence in aeronautics, maintained that an aircraft driven by a tail thrust would experience a change in the centre of gravity and flip over. Very few believed the contrary, but one of them was Ernst Heinkel. Following his offer of unhesitating support, Heinkel placed at the disposal of von Braun an He 112 fuselage shell less wings for the standing tests.[20]In 1936 von Braun had advanced far enough to begin trials. A great tongue of flame from the rocket motor roared through the fuselage tail to set up the back thrust. Late in 1936 Erich Warsitz was seconded by the RLM to Wernher von Braun and Ernst Heinkel, because he had been recognized as one of the most experienced test pilots of the time, and because he also was technically proficient.[21] Warsitz wrote:For the later flight trials Heinkel gave us an airworthy He 112 which we fitted with an additional rocket motor, and after months of untiring effort we started to look for somewhere to carry out the flight experiments under conditions of secrecy and reasonable safety.[22]The RLM agreed to lend Neuhardenberg, a large field about 70 kilometres east of Berlin, listed as a reserve airfield in the event of war. Sin

General Characteristics

  • Predecessor He112 B-0
  • Successors 1 airplane(s)
  • Created On Android
  • Wingspan 32.5ft (9.9m)
  • Length 29.3ft (8.9m)
  • Height 8.5ft (2.6m)
  • Empty Weight 14,337lbs (6,503kg)
  • Loaded Weight 24,069lbs (10,917kg)

Performance

  • Power/Weight Ratio 4.341
  • Wing Loading 30.5lbs/ft2 (149.1kg/m2)
  • Wing Area 788.1ft2 (73.2m2)
  • Drag Points 3481

Parts

  • Number of Parts 122
  • Control Surfaces 10
  • Performance Cost 460