SEARCH · Search NASA
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Discussion of the soft X-rays from Virgo observed with a scanning focusing collector from an Aerobee 170 rocket. The region included the center of the Virgo cluster of galaxies, a source of higher energies which had been previously identified with M87, and QSO 3C 273. No discrete sources in Virgo were observed.
Soft X rays in the energy regions below 284 eV and between 500 and 1000 eV have been detected on the vicinity of the North Polar Spur. The region of enhanced X-ray emission reported was observed from an Aerobee 150 rocket launched on May 29, 1970, from Woomera, Australia.
Observations of cosmic X-rays in the energy band 0.2-3.0 keV were made from an experiment on board an Aerobee 170 rocket launched from White Sands, N.M. on Dec. 19, 1970. A survey along the galactic plane between the Crab Nebula and Cygnus provided data on the interstellar absorption and X-ray flux for the Crab Nebula, NP 0532, Cas A, and Cyg X-2; upper limits were obtained for the flux from a number of supernova remnants. The 1/4 keV X-ray background was measured over a limited range of galactic latitude and longitude.
The feasibility of generating artificial auroras by injecting electrons into the upper atmosphere was investigated by using an electron accelerator aboard an Aerobee 350 rocket. Four of the artificial auroral rays were detected and recorded by two geophysical sites separated enough to enable the spatial coordinates of the rays to be determined by triangulation. It was found that (1) the beam remained well collimated; (2) most of the initial beam energy was deposited in the atmosphere; (3) plasma instabilities did not play a significant role; and (4) the orientations of the rays were determined with sufficient accuracy to improve the knowledge of the earth's magnetic field over the Virginia coast. The publications resulting from this research are listed.
The results are reported of observations in narrow bands centered on 1115, 1425, and 1446 A of the flux from an empty high-galactic-latitude region and from several stars. The observations had been obtained with the aid of three ultraviolet-sensitive Geiger counters which were carried on an Aerobee-150 rocket launched from the White Sands missile range on Mar. 13, 1969. The results obtained provide a basis for setting an upper limit to the flux from the Coma cluster of galaxies.
The far ultraviolet spectrum of the dawn airglow was observed with a scanning Ebert spectrophotometer aboard an Aerobee 170 rocket launched from White Sands, New Mexico, on January 25, 1971, at 0727 MST. Altitude profiles were obtained between 100 and 244 km for the brightest spectral features, HI 1216, OI 1304, and OI 1356. The OI 1356 column intensity is used to estimate a 1356 intensity of about 10 R at the unilluminated magnetic conjugate point; this procedure is consistent with recent observations.
An extreme ultraviolet telescope system was flown on an Aerobee 170 rocket from the White Sands Missile Range on Oct. 22, 1971. Measurements of extreme ultraviolet radiation from the night sky were made with a set of Parylene, aluminum, and tin filters behind a grazing incidence concentrator. If the aluminum and tin filter data are interpreted as being due to only the He I 584-A and He II 304-A lines, the nightglow flux at 25 deg zenith angle and 270 deg azimuth angle at 180-km altitude was I(584) = 4.4 plus or minus 1.9 R and I(304) = 1.3 plus or minus 0.5 R.
A measurement of the spatial distribution of the X-ray flux from the Perseus cluster of galaxies is reported. The measurement was made with a one-dimensional X-ray telescope carried by an Aerobee sounding rocket on February 8, 1974. The results are compared with previous X-ray observations and optical measurements of the galaxy distribution. The data show the presence of a luminous feature centered on NGC 1275, considerable emission from extended regions, and a marked asymmetry between the E-W and N-S distributions in the X-ray flux.
The absolute energy distribution in the ultraviolet is given for the stars alpha Vir, eta UMa, and alpha Leo. The calibration is based on absolute heterochromatic photometry between 2920 and 1370 A carried out with an Aerobee sounding rocket. The fundamental radiation standard is the synchrotron radiation from 240-MeV electrons in a certain synchrotron storage ring. On the basis of the sounding-rocket calibration, the preliminary OAO-2 spectrometer calibration has been revised; the fluxes for the three program stars are tabulated in energy per second per square centimeter per unit wavelength interval.
This paper reviews the history of cryogenic fluid management technology development and infusion into both the Saturn and Centaur vehicles. Ground testing and analysis proved inadequate to demonstrate full scale performance. As a consequence flight demonstration with a full scale vehicle was required by both the Saturn and Centaur programs to build confidence that problems were addressed. However; the flight vehicles were highly limited on flight instrumentation and the flight demonstration locked-in the design without challenging the function of design elements. Projects reviewed include: the Aerobee Sounding Rocket Cryogenic Fluid Management (CFM) tests which served as a valuable stepping stone to flight demonstration and built confidence in the ability to handle hydrogen in low gravity; the Saturn IVB Fluid Management Qualification flight test; the Atlas Centaur demonstration flights to develop two burn capability; and finally the Titan Centaur two post mission flight tests.
The design and performance of an Aerobee 150 rocket-borne solar spectrograph covering a wavelength range of 10 to 385 A are discussed. The spectrograph uses a gold-coated replica concave grating of 3-m radius with 1200 grooves/mm at an angle of incidence of 88 deg. The spectra are recorded on glass photographic plates making possible wavelength determination to 0.003 A if known standard wavelengths occur frequently enough. Special attention to scattered light made possible the photographing of the solar spectrum from 60 to 385 A without using filters to absorb the strong visible and UV sunlight, although the solar spectrum was also recorded through metal foil filters. In the laboratory the spectrograph has been used to record spectra of highly ionized metals with a resolution of 0.03 A or better.
Gravity preference tests on rats subjected to simulated Aerobee 150 A rocket launching and flight in ground based spiral centrifuge
The results of the first two of a series of research rocket flights are presented. The objectives of these flights were (1) to learn about the capabilities of these rockets, (2) to learn how to interface the payloads and rockets, and (3) to process some of the composite casting demonstration capsules intended originally for Apollo 15. The capsules contained experiments for investigating the stability of gas bubbles in plain and fiber-reinforced metal melted and solidified in a near-zero-g (0.0119g) environment. The characteristics of the two research rockets, an Aerobee 170A and a Black Brant VC, used to obtain the periods of near-zero-g and the temperature control unit used for processing the contents of the two experiment capsules are discussed.
Airborne instrumentation system on Aerobee 350 sounding rocket
This paper reports the observations of waves generated by a controlled beam of particles artificially injected into the ionosphere and magnetosphere. The measurements were made during the Electron Echo 1 experiment, in which an electron accelerator was carried to a height of 350 km in the ionosphere from Wallops Island, Virginia, on an Aerobee 350 sounding rocket. It injected into the earth's magnetic field over 3000 16-ms pulses of electrons with 40-keV energy and a current of 70 mA at pitch angles between 70 and 110 deg. The ejected fiber glass nose cone carried antennas and receivers to measure the electric field of waves generated by the beam. Associated with the electron beam was radiation detected at frequencies near the electron plasma frequency of the background ionosphere, near twice the electron cyclotron frequency in the whistler mode, and near zero frequency. Associated with the operation of an argon plasma generator used to keep the accelerator neutralized were continuous emissions detected at frequencies near the lower-hybrid resonance (LHR).
Aerobee payload and other instrumentation for studies in galactic X ray astronomy
Mobile Aerobee Launch Facility /MALF/, noting applications to space science
The results are summarized of reduction and analysis of data acquired during the flight of NASA-Aerobee 17.012CG. This rocket was launched from White Sands Missile Range on 6 April 1974 at 0410 U.T. The primary instrument in the experiment payload was a singly focussing x-ray reflector system sensitive in the range from 0.18 to 3 keV. X-ray detectors for this system consisted of two gas flow proportional counters with fields of view defined by apertures of 0.1 deg and 0.3 deg at the reflector focus. A Bragg spectrometer utilizing KAP crystals was included in the payload with the objective of detecting the Lyman alpha line of 0 VIII at 18.97A in the Puppis supernova remanant. A 35 mm camera photographed the star field every 1.6 sec throughout the flight to provide aspect information.