Advanced Des. Probs in Aerospc Eng. - [Vol 1 Adv. Aero. by A. Miele, et al.

By A. Miele, et al.

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In short, SSSO and SSTO configurations do not belong to the same ballpark; hence, a comparison is not meaningful. 3. SSTO versus TSTO Configurations. These configurations do belong to the same ballpark in that they require the same increase in total energy per unit weight to be placed in orbit; hence, a comparison is meaningful. Figures 5a-5d compare SSTO and TSTO configurations for the case where the latter configuration has uniform structural factor, For the Venture Star spacecraft and s, Fig.

3. , Optimal Ascent Trajectories for TSTO Spacecraft: Extensions, Aero-Astronautics Report 277, Rice University, 1997. Design of Rocket-Powered Orbital Spacecraft 29 4. , Optimal Ascent Trajectories for SSSO, SSTO, and TSTO Spacecraft: Extensions, Aero-Astronautics Report 278, Rice University, 1997. 5. ANONYMOUS, N. , Access to Space Study, Summary Report, Office of Space Systems Development, NASA Headquarters, 1994. 6. FREEMAN, D. C, TALAY, T. , STANLEY, D. , LEPSCH, R. , and WIHITE, A. 241-249, 1995.

2. , Optimal Ascent Trajectories for SSTO and TSTO Spacecraft, Aero-Astronautics Report 276, Rice University, 1997. 3. , Optimal Ascent Trajectories for TSTO Spacecraft: Extensions, Aero-Astronautics Report 277, Rice University, 1997. Design of Rocket-Powered Orbital Spacecraft 29 4. , Optimal Ascent Trajectories for SSSO, SSTO, and TSTO Spacecraft: Extensions, Aero-Astronautics Report 278, Rice University, 1997. 5. ANONYMOUS, N. , Access to Space Study, Summary Report, Office of Space Systems Development, NASA Headquarters, 1994.

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