Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv - Couverture souple

S, Prasanth ; I, Mohammed Nadhim ; Deepan C, Anto Cletus L

9786209083624: Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv

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ISBN 10 : 6209083625 ISBN 13 : 9786209083624

Editeur : LAP Lambert Academic Publishing, 2025

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�diteur: LAP Lambert Academic Publishing
Date d'�dition: 2025
Langue: anglais
ISBN 10: 6209083625
ISBN 13: 9786209083624
Reliure: Broch�
Nombre de pages: 60
Coordonn�es du fabricant: non disponible
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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv

S, Prasanth; I, Mohammed Nadhim; Deepan C, Anto Cletus L

Edit� par LAP LAMBERT Academic Publishing, 2025

ISBN 10 : 6209083625 ISBN 13 : 9786209083624

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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv

Prasanth S, Mohammed Nadhim I, Anto Cletus L Deepan C

Edit� par LAP Lambert Academic Publishing, 2025

ISBN 10 : 6209083625 ISBN 13 : 9786209083624

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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv

S, Prasanth; I, Mohammed Nadhim; Deepan C, Anto Cletus L

Edit� par LAP Lambert Academic Publishing, 2025

ISBN 10 : 6209083625 ISBN 13 : 9786209083624

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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv

S, Prasanth; I, Mohammed Nadhim; Deepan C, Anto Cletus L

Edit� par LAP LAMBERT Academic Publishing, 2025

ISBN 10 : 6209083625 ISBN 13 : 9786209083624

Neuf PAP

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PAP. Etat : New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. N� de r�f. du vendeur L0-9786209083624

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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv (Paperback)

Prasanth S.

Edit� par LAP Lambert Academic Publishing, 2025

ISBN 10 : 6209083625 ISBN 13 : 9786209083624

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Vendeur : Grand Eagle Retail, Bensenville, IL, Etats-Unis

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Paperback. Etat : new. Paperback. The project upgrades the GSLV Mk-III solid booster via a high-density composite propellant (65% bimodal AP, 18% spherical Al, 12% HTPB binder including 1.5% additives) augmented with 1% copper chromite, 1% lecithin, 1% TEPANOL and 2% iron oxide, achieving 1,795 kg/m3. An 8-lobed finocyl grain with tapered fins gives a large initial surface area for rapid pressurization and a progressiveneutral burn over 110-120 s; the grain is carbon-fiber reinforced to withstand up to 12 MPa. A flex nozzle with 0.61 m throat, 15:1 expansion (exit O 2.36 m), and a carbon-carbon throat coated with ZrC is optimized for sea-level/vacuum. Predicted performance: 5,800 kN thrust, exhaust velocity 2,714 m/s, Isp 277 s, mass flow 2,138 kg/s. This item is printed on demand. Shipping may be from multiple locations in the US or from the UK, depending on stock availability. N� de r�f. du vendeur 9786209083624

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OPTIMIZATION OF GRAIN AND NOZZLE GEOMETRY IN SOLID ROCKET BOOSTER GSLV

Prasanth S

Edit� par LAP Lambert Academic Publishing, 2025

ISBN 10 : 6209083625 ISBN 13 : 9786209083624

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Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The project upgrades the GSLV Mk III solid booster via a high density composite propellant (65% bimodal AP, 18% spherical Al, 12% HTPB binder including 1.5% additives) augmented with 1% copper chromite, 1% lecithin, 1% TEPANOL and 2% iron oxide, achieving 1,795 kg/m . An 8 lobed finocyl grain with tapered fins gives a large initial surface area for rapid pressurization and a progressive neutral burn over ~110-120 s; the grain is carbon fiber reinforced to withstand up to 12 MPa. A flex nozzle with 0.61 m throat, 15:1 expansion (exit � 2.36 m), and a carbon carbon throat coated with ZrC is optimized for sea level/vacuum. Predicted performance: 5,800 kN thrust, exhaust velocity =2,714 m/s, Isp =277 s, mass flow =2,138 kg/s. 60 pp. Englisch. N� de r�f. du vendeur 9786209083624

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Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv (Paperback)

Prasanth S.

Edit� par LAP Lambert Academic Publishing, 2025

ISBN 10 : 6209083625 ISBN 13 : 9786209083624

Neuf Paperback

impression � la demande

Vendeur : AussieBookSeller, Truganina, VIC, Australie

�valuation du vendeur 5 sur 5 �toiles

Paperback. Etat : new. Paperback. The project upgrades the GSLV Mk-III solid booster via a high-density composite propellant (65% bimodal AP, 18% spherical Al, 12% HTPB binder including 1.5% additives) augmented with 1% copper chromite, 1% lecithin, 1% TEPANOL and 2% iron oxide, achieving 1,795 kg/m3. An 8-lobed finocyl grain with tapered fins gives a large initial surface area for rapid pressurization and a progressiveneutral burn over 110-120 s; the grain is carbon-fiber reinforced to withstand up to 12 MPa. A flex nozzle with 0.61 m throat, 15:1 expansion (exit O 2.36 m), and a carbon-carbon throat coated with ZrC is optimized for sea-level/vacuum. Predicted performance: 5,800 kN thrust, exhaust velocity 2,714 m/s, Isp 277 s, mass flow 2,138 kg/s. This item is printed on demand. Shipping may be from our Sydney, NSW warehouse or from our UK or US warehouse, depending on stock availability. N� de r�f. du vendeur 9786209083624

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