Encyclopedia Astronautica
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z

X-17 HTV
Part of X-17 Family
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.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 0 km (0 mi).

1955 June 23 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: X-17. Launch Vehicle: X-17 HTV.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 20 km (12 mi).

1955 June 30 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: X-17. Launch Vehicle: X-17 HTV.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 9.00 km (5.50 mi).

1955 July 14 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: X-17. Launch Vehicle: X-17 HTV.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 10 km (6 mi).


Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2016 Mark Wade - Contact
© / Conditions for Use