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DC-XA

Launch vehicle · USA

Original archive entry. The text, images and links below are kept as they were written.

American VTOVL test vehicle. After a hard landing in the last flight of this series, the vehicle was rebuilt to the DC-XA configuration. The DC-XA flew from May 1996 until destroyed when it tipped over while landing on its fourth flight on 31 July 1996.

Country
USA
Engines
RL-10A-5
Launch Sites
White Sands
Agency
Douglas

Chronology

4 events

1996 May 18

14:20 GMT - . Launch Site: White Sands. LV Family: Delta Clipper. Launch Vehicle: DC-XA.
  • Nation: USA. Agency: NASA Huntsville. Apogee: 0 km (0 mi). First flight of the DC-XA; aeroshell caught fire during slow landing. Reached altitude of 244 m during a 62 second flight..

1996 June 7

16:15 GMT - . Launch Site: White Sands. LV Family: Delta Clipper. Launch Vehicle: DC-XA.
  • Nation: USA. Agency: NASA Huntsville. Apogee: 0 km (0 mi). Maximum structural stresses with 50% full LOX tank. Reached altitude of 590 m during a 64 second flight..

1996 June 8

18:17 GMT - . Launch Site: White Sands. LV Family: Delta Clipper. Launch Vehicle: DC-XA.
  • Nation: USA. Agency: NASA Huntsville. Apogee: 3.00 km (1.80 mi). 26-hour rapid turnaround demostration; new altitude and duration record. Reached altitude of 3140 m during a 142 second flight..

1996 July 31

19:15 GMT - . Launch Site: White Sands. LV Family: Delta Clipper. Launch Vehicle: DC-XA. FAILURE: Landing strut 2 failed to extend; vehicle tipped over and LOX tank exploded; vehicle destroyed..
  • Nation: USA. Agency: NASA Huntsville. Apogee: 1.00 km (0.60 mi). Reached altitude of 1250 m during a 140 second flight..