The design and performance of Model 2.041 quadraloop telemetry antennas for the NASA JAVELIN, Flight 12.03
Quadraloop telemetry antenna array for Javelin rocket - electrical characteristics
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Quadraloop telemetry antenna array for Javelin rocket - electrical characteristics
Function and performance of instrumentation and telemeter equipment aboard Argo D-4 Javelin rocket, flight number 8.31 DA
Javelin rocket measurements of ultraviolet radiation in airglow
VLF electric and magnetic fields observed with Javelin sounding rocket flown to 763 km, noting electromagnetic noise characteristics
Pressure profile of Javelin rocket experiment and methods for reducing gas load
VLF electric and magnetic fields observed in auroral zone with Javelin 8.46 sounding rocket
VLF electric and magnetic fields observed in auroral zone with Javelin 8.46 sounding rocket, noting HF electrostatic noise bursts
The equations for the motion, forces, and couples generated by clamshells released from spinning sounding rockets in accordance with a roll-out ejection concept are presented. The application of these equations to a study of a system for the Javelin rocket vehicle is discussed. The roll-out ejection concept advocated requires that each deploying clamshell be pivoted about an axis at its trailing edge located in the system sectioning plane. Clamshell despinning is a consequence of this deployment since the pivotal rate is in opposition to the rocket vehicle spin. The energy required by the deployment is derived largely from the rotational energy of the clamshell. Thus, the rocket vehicle will not be significantly despun by this kind of clamshell deployment. This ejection concept also permits a system design which makes it possible to limit clamshell angular motion to rotation about that one of its centroidal principal axes which is brought into parallelism with the rocket vehicle longitudinal axis. Also, by equalizing the moments of inertia about the other centroidal principal axes, the roll-out motion can be decoupled from any extraneous angular motion about these axes.
Javelin rocket soundings with far UV scanning spectrometer, noting atomic hydrogen and oxygen radiation
Energy spectra and pitch angle distributions of auroral electrons have been measured in a premidnight multiple arc auroral display by a Javelin rocket containing two identical payloads that separated in flight. The rocket was launched from Fort Churchill, Canada, at 0459 UT on March 2, 1968, and covered an altitude range up to 800 km. The electron energy spectra between 40 eV and 20 keV show a 'continuum' spectrum with a superimposed energetic peak. The center energy of the peak was observed to shift from 10-12 keV over the arcs to 2-3 keV between the arcs. This spectral structure is shown to be similar to the inverted 'V' structure reported by other investigators. The in flight separation of the two payloads allowed investigation of spatial versus temporal effects in the auroral precipitation.
Very low frequency electric and magnetic fields in ionosphere observed by Javelin 8.45
Mass spectrometer for measuring helium and hydrogen profiles in upper atmosphere, to be used with Javelin sounding rocket
Rigid body ejection dynamics of split-fairing system for four-stage Javelin sounding rocket under various parameter changes
AC electric and magnetic fields observed in ionosphere by Javelin sounding rocket
Environmental testing by Argo D-4 high altitude rocket used in fixed-frequency topside sounding to simulate conditions encountered by satellite-borne instruments
He I 584 A dayglow radiation measurement by retarding potential photoelectron analyzer on Javelin sounding rocket
Two ultraviolet photometers were flown on a Javelin sounding rocket launched from Fort Churchill, Canada, on February 18, 1970, into a weak auroral breakup. The photometers covered the wavelength bands 300-1000 A and 1050-1500 A and observed the aurora while the rocket was above the emitting regions. The observed radiations were found to originate from the visible and X-ray auroral forms recorded by ground-based all-sky cameras and onboard gas proportional X-ray counters. The intensities in the 1050- to 1500-A band were compatible with previous experimental data and available theoretical intensity calculations.
An investigation is conducted concerning the conditions encountered during a Javelin sounding rocket experiment conducted on Apr. 3, 1970 at Fort Churchill, Canada. Evidence is presented that near the equatorward edge of the auroral arc an intense beam of cold plasma ions was flowing parallel to the earth's magnetic field. The beam was associated with intense narrow band electric field oscillations near the local ion gyrofrequency. The data support the hypothesis that intense electrostatic ion cyclotron waves were driven unstable by field-aligned currents.