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L2106-3/1 [WEB APPROVED] Rocket motor, liquid fuelled combustion chamber, steel / aluminium wrapped tubes with insulation, included in flight of Dec 26 1928, Robert H Goddard, USA, 1928 (Roswell Acc No: 1958-28-12). Click to enlarge.

Rocket motor on loan from Roswell Museum and Art Center, USA

Made
  • 1928
Rocket motor, liquid fuelled combustion chamber, steel / aluminium wrapped tubes with insulation, included in flight of Dec 26 1928, Robert H Goddard, USA, 1928 (Roswell Acc No: 1958-28-12)

Summary

Object No.

L2106-3/1

Object Statement

Rocket motor, liquid fuelled combustion chamber, steel / aluminium wrapped tubes with insulation, included in flight of Dec 26 1928, Robert H Goddard, USA, 1928 (Roswell Acc No: 1958-28-12)

Physical Description

Rocket motor, liquid fuelled combustion chamber, steel / aluminium wrapped tubes with insulation, included in flight of Dec 26 1928, Robert H Goddard, USA, 1928 (Roswell Acc No: 1958-28-12)

Dimensions

Height

990 mm

Width

380 mm

Depth

350 mm

Production

Made

  • 1928

Cite this Object

Harvard

Rocket motor on loan from Roswell Museum and Art Center, USA 2020, Museum of Applied Arts & Sciences, accessed 19 September 2020, <https://ma.as/267220>

Wikipedia

{{cite web |url=https://ma.as/267220 |title=Rocket motor on loan from Roswell Museum and Art Center, USA |author=Museum of Applied Arts & Sciences |access-date=19 September 2020 |publisher=Museum of Applied Arts & Sciences, Australia}}