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
HJ Nike Nike Recruit
Part of Honest John Family
American test vehicle. Four stage vehicle consisting of 1 x M-6 + 1 x Nike + 1 x Nike + 1 x Recruit

Status: Retired 1960. First Launch: 1958-10-06. Last Launch: 1960-08-03. Number: 5 . Thrust: 365.00 kN (82,055 lbf). Gross mass: 1,300 kg (2,800 lb). Height: 10.00 m (32.00 ft). Diameter: 0.58 m (1.90 ft). Apogee: 30 km (18 mi).


More at: HJ Nike Nike Recruit.

Family: test vehicle. Country: USA. Launch Sites: Wallops Island. Stages: M-6, 1.5KS35000, M5E1. Agency: NASA Langley.

1958 October 6 - . Launch Site: Wallops Island. LV Family: Honest John. Launch Vehicle: HJ Nike Nike Recruit.
  • Polaris Re-entry Vehicle test - . Nation: USA. Agency: USN. Apogee: 26 km (16 mi).

1958 December 1 - . Launch Site: Wallops Island. LV Family: Honest John. Launch Vehicle: HJ Nike Nike Recruit.
  • Polaris Re-entry Vehicle test - . Nation: USA. Agency: USN. Apogee: 26 km (16 mi).

1959 - . Launch Site: Wallops Island. LV Family: Honest John. Launch Vehicle: HJ Nike Nike Recruit.
  • Polaris Re-entry Vehicle test - . Nation: USA. Agency: USN. Apogee: 26 km (16 mi).

1959 September 9 - . Launch Site: Wallops Island. LV Family: Honest John. Launch Vehicle: HJ Nike Nike Recruit.
  • Mercury model test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1960 August 3 - . Launch Site: Wallops Island. LV Family: Honest John. Launch Vehicle: HJ Nike Nike Recruit.
  • Glide Rocket Re-entry Vehicle test - . Nation: USA. Agency: NASA Langley. Apogee: 27 km (16 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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use