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X-17 HTV
Part of X-17
American test vehicle. Three stage vehicle consisting of 1 x 3-DS-47000 + 3 x NOTS 124-C + 1 x NOTS 124-C

Status: Retired 1955. First Launch: 1955-06-13. Last Launch: 1955-07-14. Number: 4 . Thrust: 209.00 kN (46,985 lbf). Gross mass: 100 kg (220 lb). Height: 5.00 m (16.40 ft). Diameter: 0.20 m (0.65 ft). Apogee: 10 km (6 mi).

Family: test vehicle. Country: USA. Launch Sites: Cape Canaveral, Cape Canaveral LC3. Stages: 3-DS-47000, NOTS 124-C. Agency: Lockheed.
1955 June 13 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: X-17. Launch Vehicle: X-17 HTV. FAILURE: Failure.
1955 June 23 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: X-17. Launch Vehicle: X-17 HTV.
1955 June 30 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: X-17. Launch Vehicle: X-17 HTV.
1955 July 14 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: X-17. Launch Vehicle: X-17 HTV.
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