ENAE 791 - Spring, 2008
Launch and Entry Vehicle Design
Course Syllabus and Announcements
 

  Space Systems Laboratory - Department of Aerospace Engineering - University of Maryland

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Notes and Announcements

080515 - Sorry about the delay, but all of the final lectures (including the one on the term project, which was hiding in an obscure part of my hard disk) are now posted. Good luck to those of you still working on the term project and have a nice summer!

080414 - On problem 1(d), if your deorbit burn is 1 m/sec too low (apogee velocity is 1 m/sec too high), you will find that the new orbit won't reach entry altitude at all. To allow feasible answers to (e) and (f), please change (d) to reflect a deorbit burn which is 0.5 m/sec too low.

080413 - The solutions to problem set 2 have come much slower than I wanted, as life keeps intruding into work. I have just posted solutions to questions 1-3 in the form of an Excel spreadsheet (XLS; 56 Kb, 3 pgs.) - this isn't as readable and self-explanatory as the solutions to PS1, but the time commitment required for the all-singing, all-dancing LaTeX solutions is prohibitive.

Due to the delay in these solutions, I am postponing the deadline for the midterm exam to class time on Thursday, April 17th. (And, by the way, Problem Set 3 is still on a "turn it in when you can" basis, and is clearly of secondary importance as compared to the midterm.)

080411 later - Okay, here are the solutions to problem set 1 (PDF; 4.1 Mb, 9 pgs.). I wanted to make this really clear and self-explanatory, and wound up fighting my way through LaTeX to get it done. Expect the Problem Set 2 solutions (as early tomorrow as I can) to be much less elegant.

080411 - Here's the full midterm (PDF; 64 Kb, 2 pgs.) Good luck!

080410 - I have posted the first part of the midterm - I'm still checking the final parts of the exam. The complete exam will be online tonight, but I wanted to put the first question up (which is fairly involved) so you can get started right away. Solutions to problem sets 1 and 2 will also be up shortly.

080401 - In thinking about the midterm exam, it has become clear to me that I need to do a lot more in preparation for it than I can accomplish between now and Thursday. I also think, based on the topics covered, that the midterm would be a better indicator of your understanding of the material if you could work on it in a more realistic environment than a classroom - i.e., as a take-home. Therefore, I'm going to move the midterm back one more week, and plan to hand it out on Thursday 4/10 as a takehome, which will be due by class time on Tuesday 4/15. (Just in case taxes weren't painful enough...)

Syllabus

5

 Date

 Subject

 Assignments
 Jan. 29 (#01)  Course Overview; Orbital Mechanics
 Slides (PDF: 1.98 Mb; 52 pgs.)
 Jan. 31 (#02)  Rocket Performance
 Slides (PDF: 1.94 Mb; 45 pgs.)
 Feb. 5 (#03)  Atmospheric Decay and Ballistic Entry
 Slides (PDF: 4.01 Mb, 20 pgs.)
Problem Set 1 (PDF: 113 Kb, 2 pgs.)
 Feb. 7 (#04)  Cost Estimation and Engineering Economics
 Slides (PDF: 1.1 Mb, 56 pgs.)
 Feb. 12 (#05)  Reliability, Redundancy, and Resiliency
 Slides (PDF: 1.0 Mb, 35 pgs.)
 Feb. 14 (#06)  Ballistic Entry II
Slides (PDF: 3.9 Mb, 21 pgs)
Problem Set 1 due
 Feb. 19 (#07)  Propulsion Systems
 Slides (PDF: 4.0 Mb, 47 pgs.)
 Feb. 21 (#08)  Mass Estimating Relations
 Slides (PDF: 1.2 Mb, 33 pgs.)
 Feb. 26 (#09)  Lifting Entry I
 
 Feb. 28 (#10)  Lifting Entry II; Phugoid Motion
 
 March 4  No Class
 
 March 6 (#11)  Launch Infrastructure
Problem Set 2 (PDF: 24 Kb, 2 pgs.)
Problem Set 1 solutions (partial) (PDF: 4 pgs., 383 Kb)
 March 11 (#12)  Rarified Fluids
Slides (PDF: 320 Kb, 3 pgs.)
 March 13 (#13)  Newtonian Flow; ParaShield Case Study
Problem Set 2 due
Slides (PDF: 5.2 Mb, 68 pgs.)
 March 18

 Spring Break

 March 20

 Spring Break

 
 March 25 (#14)  Entry Heating
 March 27 (#15)  Thermal Protection Systems
 
 April 1 (#16)  Sounding Rockets; Ballistic Flight
 April 3 (#17)  Case Study: Entry, Descent, and Landing
Problem Set 3 (PDF: 22 Kb, 1 pg.)
 April 8 (#18)  Gravity Turn and Optimal Launch Trajectories
 April 10 (#19)  Effects of Reusability
Midterm Exam handed out
Slides (PDF; 5.3 Mb, 43 pgs.)
 April 15 (#20)  Recitation Section
 
 April 17 (#21)  Launch Vehicle Systems
Midterm Exam due
Slides (PDF; 8.1 Mb, 41 pgs.)
 April 22  No class (work on term projects)
 April 24 (#22)  Term Project Discussion
 Slides (PDF; 3.6 Mb, 17 pgs.)
 April 29  No class (work on term projects)
 
 May 1  No class (work on term projects)
 
 May 6 (#23)  Payload Accommodations
 Slides (PDF; 3.8 Mb, 44 pgs.)
 May 8 (#24)  Failure is Always an Option
 Slides (PDF; 8.6 Mb, 28 pgs.)
 May 13 (#25)  A Rambling Wrap-up
 Slides (PDF; 2.8 Mb, 23 pgs.)