Learn · Introduction to Launch Vehicle Analysis and Design
Lecture 28 of 37Week 7
Lecture 28: Launch Widow and SSTO Concepts
Prof. Ashok Joshi · IIT Bombay
Credits and licence
- From
- Introduction to Launch Vehicle Analysis and Design, IIT Bombay (at NPTEL)
- Licence
- CC BY-NC-SA, as NPTEL states it. Non-commercial use only.
- Attribution
- NPTEL states: "Distributed under Creative Commons Attribution-ShareAlike / CC BY - NC - SA", beside a BY-NC-SA badge.
- Who can watch
- Tweens profiles and older. How courses are placed
All the lectures
- Lecture 1: Introduction
- Lecture 2: Course Plan
- Lecture 3: Ascent Mission Basics
- Lecture 4: Force and Geometry Models -1
- Lecture 5: Force and Geometry Models - 2
- Lecture 6: Idealized Performance
- Lecture 7: Trajectory Under Gravity
- Lecture 8: Impact of Gravity
- Lecture 9: Impact of Drag
- Lecture 10: Curvilinear Motion Concept
- Lecture 11: Constant Pitch Rate Solution
- Lecture 12: Constant Velocity Solution
- Lecture 13: Constant (T/m) Solution
- Lecture 14: Ascent Mission Design
- Lecture 15: Multi-stage Rocket Basics
- Lecture 16: Multi-stage Configuration Basics
- Lecture 17: Multi-stage Solution Basics
- Lecture 18: Multi-stage Problem Definition
- Lecture 19: Optimal Staging Strategy
- Lecture 20: Lagrange Solution
- Lecture 21: Approximate Staging Solution
- Lecture 22: Variant Concept
- Lecture 23: Variant Design Solution
- Lecture 24: Parallel Staging Concept
- Lecture 25: Parallel Staging Benefits
- Lecture 26: Jet Damping and Ballistic Missiles
- Lecture 27: Current Rocket Concepts
- Lecture 28: Launch Widow and SSTO Concepts
- Lecture 29: Reentry Concept
- Lecture 30: Ballistic Reentry Solution
- Lecture 31: Lifting and Other Reentry Modes
- Lecture 32: Concluding Remarks
- Lecture 33: Rectilinear Trajectories
- Lecture 34: Curvilinear Trajectories
- Lecture 35: Multi-stage Rocket Concept
- Lecture 36: Optimal Multi-stage Solutions
- Live Session 28-03-2022