Between 1993 and 1996, the McDonnell Douglas DC-X, also known as the "Delta Clipper", conducted twelve low-altitude suborbital test launches to verify the configuration and handling of the uncrewed single-stage-to-orbit Delta Clipper design, which was proposed to the United States Department of Defense and the National Aeronautics and Space Administration for use as a reuseable launch vehicle. [1] Claimed as the first rocket to conduct a vertical landing on Earth, the DC-X was a one-third scale demonstrator for the proposed operational Delta Clipper vehicle. [2]
After the first three flights Strategic Defense Initiative Organization funding for the test project was cancelled; [3] the remaining test program was conducted by NASA and the Advanced Research Projects Agency. [4] Following the eighth test flight, the vehicle was transferred fully to NASA and the vehicle was modified to DC-XA configuration, [5] also known as "Clipper Graham" after General Daniel O. Graham who had died in 1995 after supporting the Delta Clipper project. [6]
Of the overall test program, ten of the vehicle's launches were fully successful; the fifth test flight was aborted early in the flight following an on-board explosion but the vehicle was successfully recovered. The twelfth and final flight saw one of the vehicle's landing legs fail to extend; on landing, when the vehicle tipped over onto its unsupported corner, a liquid oxygen tank ruptured and exploded, the ensuing fire destroying the modified DC-XA vehicle and ending the program. Despite the loss the program was considered overall to have been a success. [1]
Flight No. | Date and time of takeoff (UTC) | Vehicle | Launch site | Suborbital apogee | Outcome | Duration | Reference |
---|---|---|---|---|---|---|---|
1 | 18 August 1993 23:43 | DC-X | White Sands Space Harbor | 46 m (151 ft) | Success | 59 sec | [7] |
Control system and vertical landing capability test. [7] Demonstrated hovering ability and 350 foot (110 m) horizontal translation. [6] | |||||||
2 | 11 September 1993 18:12 | DC-X | White Sands Space Harbor | 92 m (302 ft) | Success | 66 sec | [7] |
Ground effects and ascent-and-landing mode control test. [7] | |||||||
3 | 30 September 1993 17:30 | DC-X | White Sands Space Harbor | 370 m (1,210 ft) | Success | 72 sec | [7] |
Aerostability test; vehicle conducted 180° roll. [7] | |||||||
4 | 20 June 1994 15:42 | DC-X | White Sands Space Harbor | 870 m (2,850 ft) | Success | 2 min 16 sec | [7] |
First flight with fully loaded propellant tanks and operational radar altimeter. [7] | |||||||
5 | 27 June 1994 15:37 | DC-X | White Sands Space Harbor | 790 m (2,590 ft) | Partial failure | 78 sec | [7] |
Flight aborted after hydrogen explosion on launch; autoland capabilities demonstrated. [7] | |||||||
6 | 16 May 1995 16:40 | DC-X | White Sands Space Harbor | 1.33 km (0.83 mi; 4,400 ft) | Success | 2 min 4 sec | [7] |
Flight envelope expansion test. [7] | |||||||
7 | 12 June 1995 15:38 | DC-X | White Sands Space Harbor | 1.74 km (1.08 mi; 5,700 ft) | Success | 2 min 12 sec | [7] |
AOA envelope expansion, first reaction control system usage. [7] | |||||||
8 | 7 July 1995 14:02 | DC-X | White Sands Space Harbor | 2 km (1.2 mi; 6,600 ft) | Success | 2 min 4 sec | [7] |
Turnaround maneuver demonstrated; hard landing resulted in damage to the aeroshell. [7] | |||||||
9 | 18 May 1996 15:14 | DC-XA | White Sands Space Harbor | 244 m (801 ft) | Success | 62 sec | [7] |
First flight following modification to DC-XA configuration; slow landing resulted in aeroshell fire. [7] | |||||||
10 | 7 June 1996 17:15 | DC-XA | White Sands Space Harbor | 590 m (1,940 ft) | Success | 64 sec | [7] |
Maximum structural stress test. [7] | |||||||
11 | 8 June 1996 19:17 | DC-XA | White Sands Space Harbor | 3.14 km (1.95 mi; 10,300 ft) | Success | 2 min 22 sec | [7] |
Demonstration of 26-hour rapid turnaround; altitude and duration record set. [7] | |||||||
12 | 31 July 1996 20:15 | DC-XA | White Sands Space Harbor | 1.25 km (0.78 mi; 4,100 ft) | Partial success | 2 min 20 sec | [7] |
Successful maneuvering test; vehicle destroyed on landing when landing strut failed to extend and LOX tank exploded. [7] [8] |
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