Proceedings of the XXth International Astronautical Congress
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9780080168418

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DISPOSITIF DE CONTRÔLE D'ATTITUDE CASSIOPÉE: PREMIERS ESSAIS EN VOL

Proceedings of the XXth International Astronautical Congress ◽

10.1016/b978-0-08-016841-8.50048-1 ◽

1972 ◽

pp. 779-785

Author(s):

A. REMONDIÈRE

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COMPARISON OF THEORETICAL AND EXPERIMENTAL ATTITUDE DATA FOR THE DODGE SPACECRAFT

Proceedings of the XXth International Astronautical Congress ◽

10.1016/b978-0-08-016841-8.50047-x ◽

1972 ◽

pp. 759-778

Author(s):

J.M. WHISNANT ◽

V.L. PISACANE

Keyword(s):

Experimental Attitude

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DATA TRANSMISSION FOR PLANETARY STUDIES

Proceedings of the XXth International Astronautical Congress ◽

10.1016/b978-0-08-016841-8.50044-4 ◽

1972 ◽

pp. 711-723

Author(s):

Y.K. KHODAREV

Keyword(s):

Data Transmission

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PREDICTION OF THERMAL FLUXES TO VERY BLUNT PLANETARY ENTRY VEHICLES BY THE INTEGRAL METHOD

Proceedings of the XXth International Astronautical Congress ◽

10.1016/b978-0-08-016841-8.50030-4 ◽

1972 ◽

pp. 455-479

Author(s):

R.K. BURNS ◽

C.C. OLIVER

Keyword(s):

Integral Method ◽

Planetary Entry

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SCIENTIFIC RESULTS OBTAINED IN THE FLIGHTS OF THE AUTOMATIC IONOSPHERIC LABORATORIES YANTAR

Proceedings of the XXth International Astronautical Congress ◽

10.1016/b978-0-08-016841-8.50029-8 ◽

1972 ◽

pp. 445-454b

Author(s):

L.A. ARTSIMOVICH ◽

G.L. GRODZOVSKII YU ◽

I. DANILOV ◽

V.M. ZAKHAROV ◽

N.F. KRAVTSEV ◽

...

Keyword(s):

Scientific Results

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REMOTE MANIPULATOR SPACECRAFT SYSTEMS

Proceedings of the XXth International Astronautical Congress ◽

10.1016/b978-0-08-016841-8.50014-6 ◽

1972 ◽

pp. 189-207c

Author(s):

A. INTERIAN ◽

R.H. BLACKMER ◽

W.H. ALLEN

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THE ORBITING GEOPHYSICAL OBSERVATORIES

Proceedings of the XXth International Astronautical Congress ◽

10.1016/b978-0-08-016841-8.50010-9 ◽

1972 ◽

pp. 131-138b

Author(s):

W.E. SCULL

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FUTURE LAUNCH VEHICLE WITH MULTI-MISSION CAPABILITY, USING HIGH ENERGY PROPULSION SYSTEMS

Proceedings of the XXth International Astronautical Congress ◽

10.1016/b978-0-08-016841-8.50007-9 ◽

1972 ◽

pp. 55-73b

Author(s):

R. REICHERT

Keyword(s):

High Energy ◽

Launch Vehicle ◽

Propulsion Systems

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Front Matter

Proceedings of the XXth International Astronautical Congress ◽

10.1016/b978-0-08-016841-8.50001-8 ◽

1972 ◽

pp. iii

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EDITOR'S NOTE

Proceedings of the XXth International Astronautical Congress ◽

10.1016/b978-0-08-016841-8.50063-8 ◽

1972 ◽

pp. 985

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Proceedings of the XXth International Astronautical CongressLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By Elsevier

DISPOSITIF DE CONTRÔLE D'ATTITUDE CASSIOPÉE: PREMIERS ESSAIS EN VOL

COMPARISON OF THEORETICAL AND EXPERIMENTAL ATTITUDE DATA FOR THE DODGE SPACECRAFT

DATA TRANSMISSION FOR PLANETARY STUDIES

PREDICTION OF THERMAL FLUXES TO VERY BLUNT PLANETARY ENTRY VEHICLES BY THE INTEGRAL METHOD

SCIENTIFIC RESULTS OBTAINED IN THE FLIGHTS OF THE AUTOMATIC IONOSPHERIC LABORATORIES YANTAR

REMOTE MANIPULATOR SPACECRAFT SYSTEMS

THE ORBITING GEOPHYSICAL OBSERVATORIES

FUTURE LAUNCH VEHICLE WITH MULTI-MISSION CAPABILITY, USING HIGH ENERGY PROPULSION SYSTEMS

Front Matter

EDITOR'S NOTE

Proceedings of the XXth International Astronautical Congress
Latest Publications