TY - GEN
T1 - Analysis of the first stage trajectory for atsto space transportation concept powered by rbcc engine
AU - Xue, Rui
AU - Hu, Chunbo
AU - Lv, Xiang
AU - Qint, Fei
PY - 2012
Y1 - 2012
N2 - Reusable hypersonic space transportation powered by RBCC engine was described. Taking one Two-Stage-To-Orbit(TSTO) concept flight vehicle and one national RBCC experimental engine as research object. Based on the equations of dynamics and kinematics, numerical integral was used to design the trajectory. The simulation of the trajectory of the first stage flight vehicle powered by RBCC engine in a TSTO hypersonic space transportation is made by MATLAB. The result of simulation experiment shows that the model and the calculation method are feasible, which can be applied as the evaluation of the feasibility of hypersonic space transportation concepts ; the mass flow rate of fuel needed in this climb trajectory can be solved. Through these results can evaluate the acceleration performance of the RBCC engine being developed in our country, and they can also provide a direction to the development of RBCC engine in our country.
AB - Reusable hypersonic space transportation powered by RBCC engine was described. Taking one Two-Stage-To-Orbit(TSTO) concept flight vehicle and one national RBCC experimental engine as research object. Based on the equations of dynamics and kinematics, numerical integral was used to design the trajectory. The simulation of the trajectory of the first stage flight vehicle powered by RBCC engine in a TSTO hypersonic space transportation is made by MATLAB. The result of simulation experiment shows that the model and the calculation method are feasible, which can be applied as the evaluation of the feasibility of hypersonic space transportation concepts ; the mass flow rate of fuel needed in this climb trajectory can be solved. Through these results can evaluate the acceleration performance of the RBCC engine being developed in our country, and they can also provide a direction to the development of RBCC engine in our country.
UR - http://www.scopus.com/inward/record.url?scp=84883535964&partnerID=8YFLogxK
M3 - 会议稿件
AN - SCOPUS:84883535964
SN - 9781622769797
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 7732
EP - 7737
BT - 63rd International Astronautical Congress 2012, IAC 2012
T2 - 63rd International Astronautical Congress 2012, IAC 2012
Y2 - 1 October 2012 through 5 October 2012
ER -