The Incremental Development of a Cost-Effective Small Launch Vehicle for Nanosat Payloads

Author:

Garvey John1,Besnard Eric2,Elson Geoff3,Carter Kelly3

Affiliation:

1. Garvey Spacecraft Corporation

2. California State University

3. California State University Long Beach

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

1. In the very near term, the CALVEIN team plans to re-fly its Prospector 3 vehicle to continue development of TVC capabilities. In parallel, the team is now generating the two-stage NLV concept, which is anticipated to be finished by the end of this year. Candidate follow-on tasks for early 2004 include development of next generation TVC subsystems, a full-scale first prototype and and/or possibly the 5,000 Ibf-classengine.

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1. An improved scheme of air temperature conditioning for payload fairing of ultralight space rockets;XLV ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S.P. KOROLEV AND OTHER OUTSTANDING NATIONAL SCIENTISTS — PIONEERS OF SPACE EXPLORATION;2023

2. Rapid Turn-Around Flight Testing of a Next-Generation Prototype RLV;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21

3. Development and Testing of a Prototype LOX/Propylene Upper Stage Engine;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21

4. Using Small Launch Vehicles and Microsatellites to Provide Students a True Systems Integration Experience;AIAA Space 2003 Conference & Exposition;2003-06-26

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