ISBN: 9786209102691 - reusability of gslv mk iii solid boosters using falcon 9: inspired techniques (11 risultati)

Condizione: New.

Condizione: New.

Taschenbuch. Condizione: Neu. REUSABILITY OF GSLV MK III SOLID BOOSTERS USING FALCON 9 | INSPIRED TECHNIQUES | Prasanth S (u. a.) | Taschenbuch | Englisch | 2025 | LAP LAMBERT Academic Publishing | EAN 9786209102691 | Verantwortliche Person für die EU: SIA OmniScriptum Publishing, Brivibas Gatve 197, 1039 RIGA, LETTLAND, customerservice[at]vdm-vsg[dot]de | Anbieter: preigu.…

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

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

Taschenbuch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware 68 pp. Englisch.

Taschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Advancements in global space launch technology call for India's launch vehicles to become more reusable and versatile. This project proposes redesigning the GSLV Mk3 by replacing S200 solid boosters with reusable LOX/kerosene boosters and adding boost-back and vertical landing to the first stage. The second stage is optimized for partial or full recovery, while the C25 cryogenic upper stage is upgraded for better efficiency to support GTO, LEO, and interplanetary missions. Calculations cover thrust, mass ratios, specific impulse, gravity and drag losses, and overall Deltav budgets. Trajectory simulations using GPOPS-II optimize ascent profiles and reduce performance losses. Structural analysis ensures vehicle integrity under aerodynamic and re-entry stresses. Focus is on lightweight materials, improved thermal protection, and aerodynamic control for precision landing. This redesign aims to lower costs, increase launch frequency, and expand ISRO's mission capabilities. Challenges include thermal management, hypersonic control, and landing reliability. The project envisions next-generation Indian launch vehicles with global competitiveness and sustainable space access.…

Condizione: New. Print on Demand.

Paperback. Condizione: new. Paperback. Advancements in global space launch technology call for India's launch vehicles to become more reusable and versatile. This project proposes redesigning the GSLV Mk3 by replacing S200 solid boosters with reusable LOX/kerosene boosters and adding boost-back and vertical landing to the first stage. The second stage is optimized for partial or full recovery, while the C25 cryogenic upper stage is upgraded for better efficiency to support GTO, LEO, and interplanetary missions. Calculations cover thrust, mass ratios, specific impulse, gravity and drag losses, and overall Dv budgets. Trajectory simulations using GPOPS-II optimize ascent profiles and reduce performance losses. Structural analysis ensures vehicle integrity under aerodynamic and re-entry stresses. Focus is on lightweight materials, improved thermal protection, and aerodynamic control for precision landing. This redesign aims to lower costs, increase launch frequency, and expand ISRO's mission capabilities. Challenges include thermal management, hypersonic control, and landing reliability. The project envisions next-generation Indian launch vehicles with global competitiveness and sustainable space access. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability.…

Condizione: New. PRINT ON DEMAND.

Taschenbuch. Condizione: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Advancements in global space launch technology call for India's launch vehicles to become more reusable and versatile. This project proposes redesigning the GSLV Mk3 by replacing S200 solid boosters with reusable LOX/kerosene boosters and adding boost-back and vertical landing to the first stage. The second stage is optimized for partial or full recovery, while the C25 cryogenic upper stage is upgraded for better efficiency to support GTO, LEO, and interplanetary missions. Calculations cover thrust, mass ratios, specific impulse, gravity and drag losses, and overall ¿v budgets. Trajectory simulations using GPOPS-II optimize ascent profiles and reduce performance losses. Structural analysis ensures vehicle integrity under aerodynamic and re-entry stresses. Focus is on lightweight materials, improved thermal protection, and aerodynamic control for precision landing. This redesign aims to lower costs, increase launch frequency, and expand ISRO's mission capabilities. Challenges include thermal management, hypersonic control, and landing reliability. The project envisions next-generation Indian launch vehicles with global competitiveness and sustainable space access.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 68 pp. Englisch.…