Search NASA⌕ Search

Engineering topics

Kerzhanovich, V.

Publications and source records attributed to Kerzhanovich, V..

At least 19 records
All sourcesNASA NTRSDOE OSTI
NASA NTRS2003

Low-cost balloon missions to Mars and Venus

The first successful flight demonstration of aerial deployment of Mars balloon prototypes in June 2002 and, earlier, of Venus balloon prototype deemed to be a turning point in the risk assessment of balloon missions.

balloons Mars Venus↗
NASA NTRS2002

Titan airship explorer

Explore the source record for details and available documents.

in situ sample return Saturn radioisotope thermal ↗
NASA NTRS2001

Recent progress in planetary balloons

In the last 15 years several balloon mission concepts have been proposed for Mars and Venus, one of them - Russian-French Mars Aerostat - was extensively developed in 1988-1995 but was terminated before completion.

planets balloons aerobots↗
NASA NTRS2001

Titan Airship Surveyor

Saturn's moon Titan is considered to be one of the prime candidates for studying prebiotic materials - the substances that precede the formation of life but have disappeared from the Earth as a result of the evolution of life. A unique combination of a dense, predominantly nitrogen, atmosphere (more than four times that of the Earth), low gravity (six times less than on the Earth) and small temperature variations makes Titan the almost ideal planet for studies with lighter-than-air aerial platforms (aerobots). Moreover, since methane clouds and photochemical haze obscure the surface, low-altitude aerial platforms are the only practical means that can provide global mapping of the Titan surface at visible and infrared wavelengths. One major challenge in Titan exploration is the extremely cold atmosphere (approx. 90 K). However, current material technology the capability to operate aerobots at these very low temperatures. A second challenge is the remoteness from the Sun (10 AU) that makes the nuclear (radioisotopic) energy the only practical source of power. A third challenge is remoteness from the Earth (approx. 10 AU, two-way light-time approx. 160 min) which imposes restrictions on data rates and makes impractical any meaningful real-time control. A small-size airship (approx. 25 cu m) can carry a payload approximately 100 kg. A Stirling engine coupled to a radioisotope heat source would be the prime choice for producing both mechanical and electrical power for sensing, control, and communications. The cold atmospheric temperature makes Stirling machines especially effective. With the radioisotope power source the airship may fly with speed approximately 5 m/s for a year or more providing an excellent platform for in situ atmosphere measurements and a high-resolution remote sensing with unlimited access on a global scale. In a station-keeping mode the airship can be used for in situ studies on the surface by winching down an instrument package. Floating above the surface allows relatively simple means for flight control. Mission requirements and possible methods of navigation, control, data acquisition, and communications are discussed. The presentation describes also the state-of-the art and current progress in aerial deployed aerobots.

Kerzhanovich, V.↗
NASA NTRS2000

Martian aerobot missions: first two generations

Role of aerobot missions as a new vehicle for Mars exploration have been emphasized at the recent NASA Workshop on Concepts Recent and Approaches for Mars Exploration. Unique combination of proximity to the surface and mobility with elimination of the landing makes aerobots a vital component of Mars investigation.

Mars aerobots↗
NASA NTRS2000

Balloons for planetary exploration

Robotic Balloons (Aerobots) may significantly change the future of in situ planetary exploration. On Mars, the aerobots can fill the gap in resolution/coverage between the orbiters and rovers.

balloons planetary exploration↗
NASA NTRS2000

Exploration of Mars Using Aerial Platforms

The exploration of the atmosphere of Mars can be conducted using aerial platforms such as balloons and airships. Current research and development efforts at NASA include a lobed pressurized balloon system for the Ultra Long Duration Balloon Program. The capabilities of this system, in regards to pressure, load carrying capability, and duration, are far greater than anything previously flown. This technology can be adapted for use in the atmosphere of Mars.

Fairbrother, D. A.↗
NASA NTRS2000

Mars Aerobot Missions

Mars aerobots constitute a class of mission nearly a factor of 10 smaller than earlier concepts for Mars balloons. A key goal is to achieve high payload mass fraction in a small total systems mass and to maximize the scientific potential of that payload. The "low and slow" attributes of aerobot flight paths afford advantages for many observations and measurements of Mars. Scientific objectives include surveys of remnant magnetism, studies of the surface with high resolution stereo imaging, and investigations of the structure and dynamics of the atmosphere with an in situ meteorology payload.

Greeley, R.↗