'Ballistic coefficient' presentation slideshows

Michael Skeen Ryan Starkey University of Colorado at Boulder

Conceptual Modeling and Analysis of Drag-Augmented Supersonic Retropropulsion for Application in Mars Entry, Descent, and Landing Vehicles. Michael Skeen Ryan Starkey University of Colorado at Boulder Department of Aerospace Engineering Sciences 10 th International Planetary Probe Workshop

554 views • 40 slides

Thrust, Balance, Pressure

586 views • 37 slides

Engineering Concepts Thrust, Balance, Pressure

531 views • 37 slides

Thrust, Balance, Pressure

391 views • 37 slides

Trajectory Code Validation Slides 04/12/08

407 views • 22 slides

Atul Kumar Presentation Week 3: February 1 st , 2007

Atul Kumar Presentation Week 3: February 1 st , 2007. Aerodynamics Team Re-Entry vehicle analysis - Lifting body. 1. Mass calculations. Mass and Volume of the payload. For transfer from HMO to the surface of Mars at the end of 2 nd synodic period.

296 views • 16 slides

ENGR404 : Introduction to Space Systems and Spacecraft Design University of Idaho

Good Things in SMAD. ENGR404 : Introduction to Space Systems and Spacecraft Design University of Idaho. Good Things in SMAD. Tables in back of book. 2. ENGR404 : Introduction to Space Systems and Spacecraft Design University of Idaho. Good Things in SMAD. Tables in back of book. 3.

254 views • 9 slides

Low Ballistic Coefficient Re-Entry Probe

Low Ballistic Coefficient Re-Entry Probe. K. Ramus (kevinramus@vandals.uidaho.edu) 1 , B. Holmes 1 , A. Camery 1 , D. Eld 1 , R . Riggs 1 , R. Gunn 1 , D.H . Atkinson 1 , M . Murbach 2 , and the Univ. I daho RISE Student Launch Team 1

143 views • 1 slides