Journeyman Media Gallery

5 stage vehicle of the Argo series consisting of 2 x Recruit + 1 x Sergeant + 1 x Lance + 1 x Lance + 1 x Altair

From NASA SOUNDING ROCKETS, 1958-1968 - A Historical Summary, NASA SP-4401, 1971, by William R. Corliss

During the first year of the existence of Goddard's Sounding Rocket Branch, several sounding rockets, whose development predated NASA, came into the "stable" of vehicles readily available to NASA. Chief among these were the Javelin and Journeyman, both in the so-called Argo series. The Argo series was developed by the Aerolab Development Co. under the sponsorship of NACA/NASA, with support from the Air Force Special Weapons Center, the Naval Bureau of Ordnance, and the Allegany Ballistics Laboratory.

The Argo vehicles were derived from a family of NACA/NASA hypersonic test vehicles, after the fashion of the Nike-Deacon and Nike-Cajun. Aerolab has designed a long series of Argo rockets, including the Argo E-20, designed to lift 4.5 kg (10 lb) to 24 384 m (80 000 ft); but only the Jason (Argo E-5), the Javelin (Argo D-4), and the Journeyman (Argo D-8) have seen significant use. NASA never employed the Jason, but it is the rocket that the Air Force employed to measure high-altitude nuclear radiation during the Argus experiments in the late summer of 1958, when nuclear weapons were exploded at high altitudes. NASA has used the Javelin to some extent. The Journeyman helped NASA gather radiation data prior to the Mercury flights and has also seen some Air Force use. In general, the Argos are rather large by sounding rocket standards. They were all put together from off-the-shelf military hardware, often following vehicle adaptations by Langley Research Center. NASA use of the Argo series has been minimal.

Manufacturer: Aerolab. Launches: 8. First Launch Date: 1960-09-19. Last Launch Date: 1965-06-30. Launch data is: complete. Apogee: 3,000 km (1,800 mi). Total Mass: 6,300 kg (13,800 lb). Core Diameter: 0.79 m (2.59 ft). Total Length: 18.90 m (62.00 ft).

1960 September 19 - 16:35 GMT - Launch Site: Point Arguello. Launch Complex: LC-A. Launch Vehicle: Journeyman. LV Configuration: Journeyman NASA 11.01GE.

• NERV I Cosmic rays mission Nation: USA. Agency: NASA. Apogee: 1,884 km (1,170 mi). References: 1592.

• BIOS I biological mission Nation: USA. Agency: NASA. Apogee: 1,057 km (656 mi). References: 1592.

• BIOS I biological mission Nation: USA. Agency: NASA. Apogee: 1,057 km (656 mi). References: 1592.

• Magnetospheric mission? Nation: USA. Agency: AEC. Apogee: 1,500 km (900 mi). References: 916.

• Radio Astronomy mission Nation: USA. Agency: NASA. Apogee: 1,691 km (1,050 mi). References: 1592.

• Electron Spectrometer Magnetospheric mission Nation: USA. Agency: NASA. Apogee: 1,675 km (1,040 mi). References: 1592.

• Plasma mission Nation: USA. Agency: NASA. Apogee: 1,660 km (1,030 mi). References: 1592.

• Radio Astronomy mission Nation: USA. Agency: NASA. Apogee: 1,770 km (1,090 mi). References: 1592.

• McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.