9786209083624 - Optimization of Grain and Nozzle Geometry in Solid Rocket Booster Gslv de S, Prasanth; I, Mohammed Nadhim; Deepan C, Anto Cletus L (15 resultados)

Paperback. Condición: New.

Condición: New.

Condición: New.

Taschenbuch. Condición: Neu. OPTIMIZATION OF GRAIN AND NOZZLE GEOMETRY IN SOLID ROCKET BOOSTER GSLV | Prasanth S (u. a.) | Taschenbuch | Englisch | 2025 | LAP LAMBERT Academic Publishing | EAN 9786209083624 | Verantwortliche Person für die EU: SIA OmniScriptum Publishing, Brivibas Gatve 197, 1039 RIGA, LETTLAND, customerservice[at]vdm-vsg[dot]de | Anbieter: preigu.

Paperback. Condición: New.

PAP. Condición: New. New Book. Shipped from UK. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.

PAP. Condición: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000.

Paperback. Condición: 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.

Taschenbuch. Condición: 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 Ø 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.

Paperback. Condición: 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.

Condición: New. Print on Demand.

Condición: New. PRINT ON DEMAND.

Paperback. Condición: 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 UK warehouse or from our Australian or US warehouses, depending on stock availability.

Taschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. 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 Ø 2.36 m), and a carbon¿carbon throat coated with ZrC is optimized for seälevel/vacuum. Predicted performance: 5,800 kN thrust, exhaust velocity ¿2,714 m/s, Isp ¿277 s, mass flow ¿2,138 kg/s.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 60 pp. Englisch.

Taschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - 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 Ø 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.