Engineering topics

Stern, S. A.

Publications and source records attributed to Stern, S. A..

44 records · Page 3

NASA NTRS1989

Structure/permeability relationships of silicon-containing polyimides

The permeability to H2, O2, N2, CO2 and CH4 of three silicone-polyimide random copolymers and two polyimides containing silicon atoms in their backbone chains, was determined at 35.0 C and at pressures up to about 120 psig (approximately 8.2 atm). The copolymers contained different amounts of BPADA-m-PDA and amine-terminated poly (dimethyl siloxane) and also had different numbers of siloxane linkages in their silicone component. The polyimides containing silicon atoms (silicon-modified polyimides) were SiDA-4,4'-ODA and SiDA-p-PDA. The gas permeability and selectivity of the copolymers are more similar to those of their silicone component than of the polyimide component. By contrast, the permeability and selectivity of the silicon-modified polyimides are more similar to those of their parent polyimides, PMDA-4,4'-ODA and SiDA-p-PDA. The substitution of SiDA for the PMDA moiety in a polyimide appears to result in a significant increase in gas permeability, without a correspondingly large decrease in selectivity. The potential usefulness of the above polymers and copolymers as gas separation membranes is discussed.

Stern, S. A.↗

NASA NTRS1988

The Pluto-Charon system - The escape of Charon's primordial atmosphere

Although Charon seems to have lost its atmosphere and surface volatiles, a lack of heating that would be sufficient to generate melting and consequent separation of the lighter and heavier nonvolatiles has probably resulted in the outer layers' retention of the primordial mix of nonvolatiles. Spectroscopically-determined relative abundances for the Charon surface should accordingly be representative of its entire mass, and thereby constitutes the basis of an understanding of Charon's origin. The study of Charon's exposed nonvolatile ices may ascertain whether the Pluto-Charon system condensed out of the solar nebula directly or from a protoplanetary nebula.

Trafton, L.↗

NASA NTRS1988

Mars orbital tethered sample return: The feasibility and uses of obtaining entrained particulates from the atmosphere

By employing technology developed for the Tethered Satellite Program, it appears feasible to obtain Martian dust samples from the atmosphere using an orbiting spacecraft. If collected during an annual dust storm, such a sample would contain a global selection of windborne materials. Atmospheric dust sampling is of importance to the study of Martian surface geochemistry, soil mechanics, atmospheric dynamics, and atmospheric and radiative transfer. Tethered sample return offers two key advantages over a lander sample return: relative simplicity and low spacecraft weight. In another vein, the collection of atmospheric dust by a lander sample return mission is itself of scientific merit. By employing a mast and collection plate aboard a lander mission, it is possible to obtain dust from distant locations transported as entrained material in the local aeolian environment.

Stern, S. A.↗

NASA NTRS1987

Inadequacy of single-impulse transfers for path constrained rendezvous

The use of single-impulse techniques to maneuver from point to point about a large space structure (LSS) with an arbitrary geometrical configuration and spin is examined. Particular consideration is given to transfers with both endpoints on the forbidden zone surface. Clohessy-Wiltshire equations of relative motion are employed to solve path constrained rendezvous problems. External and internal transfers between arbitrary points are analyzed in terms of tangential departure and arrival conditions. It is observed that single-impulse techniques are inadequate for transferring about the exterior of any LSS; however, single-impulse transfers are applicable for transfers in the interior of LSSs. It is concluded that single-impulse transducers are not applicable for path constrained rendezvous guidance.

Stern, S. A.↗

NASA NTRS1986

Path-constrained rendezvous - Necessary and sufficient conditions

The problem of path-constrained rendezvous in the vicinity of a Large Space Structure (LSS) was first introduced some years ago. The present contribution to this field centers on a demonstration that the problem can be reduced from a path-constraint problem to one of end-point constraints or certain (common) LSS geometries, under the assumption of an unrestrictive upper limit on the transfer time. This finding has been made under the assumption of a circular Keplerian orbit, and has been normalized with respect to orbital semimajor axis and LSS size. In addition to demonstrating this important simplification of the path-constrained rendezvous problem, the results of numerical simulations of path-constrained transfers from point-to-point on large spherical structures in orbit are discussed, and a series of conclusions having both architectural (design) and operational implications for LSS designers/operators is derived.

Soileau, K. M.↗

NASA NTRS1985

Operational implications for path constrained rendezvous

After noting that many large orbiting space structures will be of such magnitude as to require proximity rendezvous guidance targeting in order to accomplish path-constrained approaches in the vicinity of their exterior surfaces, attention is given to the difficulties that inhere in the accomplishment of such rendezvous transfers due to physical constraints imposed by the structures' surfaces. Operationally feasible transfer techniques which circumvent the path constraints inherent in these maneuvers are discussed under the assumption of a number of restrictions. The techniques presented may be important in asteroid exploration and exploitation.

Stern, S. A.↗

NASA NTRS1984

Constraints on bulk composition, seasonal variation, and global dynamics of Pluto's atmosphere

The potential seasonal variation of Pluto's atmosphere is investigated by considering the behavior of the candidate atmospheric constituents Ne, N2, CO, O2, and Ar when individually mixed with CH4. The effects of diurnal and latitudinal variation of insolation and eclipses on the atmosphere are also studied. Seasonal effects are shown to dominate. It is shown that the atmospheric bulk may not be a minimum near aphelion but rather at intermediate distances from the sun during summer/winter where inadequate ice deposits may allow the atmosphere to collapse by freezing out over winter latitudes. The likely global circulation regimes for each model atmosphere are investigated as a function of temperature, and it is concluded that if CH4, O2, or CO dominates the atmosphere, Pluto will exhibit cyclic variations between an axially symmetric circulation system at perihelion and a baroclinic wave regime at aphelion. If N2 dominates the wave regime should hold continuously.

Stern, S. A.↗

NASA NTRS1983

On the global distribution of Pluto's atmosphere

The present investigation is relevant to the study of Pluto's current global and diurnal radiation balance. Strong gravitational tides are suggested by Charon's close proximity to Pluto (approximately 20,000 km) and Charon's large relative mass (roughly 0.25 Pluto's mass). Thus, the Pluto-Charon system replaces the earth-moon system as the best known example of a double planet. Methane is the only gas positively detected in Pluto's atmosphere. The tendency of the whole atmosphere to bulge preferentially toward the subsolar point as a result of the solar heating of the suface is considered, taking into account the longitudinal and the latitudinal tide. It is concluded that near perihelion, Pluto's atmosphere is essentially uniform over Pluto's surface. Its heat capacity by virtue of the heat of condensation is large enough that eclipses and the diurnal variation of insolation cause negligible freezing out of atmospheric gases.

Trafton, L.↗