Ascent, Stage Separation and Glideback Performance of a Partially Reusable Small Launch Vehicle-Reference-Cited by-同舟云学术

Ascent, Stage Separation and Glideback Performance of a Partially Reusable Small Launch Vehicle

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Pamadi Bandu¹,Tartabini Paul¹,Starr Brett¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-876

Reference14 articles.

1. Naftel, J.C., Powell, R.W., Analysis of the Staging Maneuver and Booster Glideback Guidance for a Two-Stage, Winged, Fully Reusable Launch Vehicle,NASATP3335,1993.

2. Brauer, G.L., Cornick, D.E., and Stevenson, R., Capabilities and Applications of the Program to Optimize Simulated Trajectories, NASA CR-2770, February1977.

3. UsingADAMS/Solver,MechanicalDynamics,Inc.,1999.

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. United Trajectory Design Method for Return to Launch Site of Suborbital Reusable Launch Vehicle;21st AIAA International Space Planes and Hypersonics Technologies Conference;2017-03-02

2. Effective fault diagnosis based on strong tracking UKF;Aircraft Engineering and Aerospace Technology;2011-09-06

3. Integrated Navigation for Flyback Reusable Booster Vehicles;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2011

4. Simulation and Analyses of Stage Separation of Two-Stage Reusable Launch Vehicles;AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference;2005-05-16

5. Aerodynamic Characteristics and Glide-Back Performance of Langley Glide-Back Booster;22nd Applied Aerodynamics Conference and Exhibit;2004-06-20