solid propellant space launch vehicle development program for peru – a proposal
- Paper number
IAC-14,D2,7,8,x26789
- Author
Dr. Fredy Villanueva, Conida - Space Agency of Peru, Peru
- Year
2014
- Abstract
A family of solid propellant space launch vehicles (SLV) is proposed based on the indigenous technology development evolution. Each LV design model has been optimized, a multidisciplinary design optimization framework has been applied. The proposed SLVs are intended to deliver a small payload of 100 - 200 kg into a low earth orbit of 600 - 800 km altitude. A multi discipline feasible integrated framework has been implemented among the aerodynamic, propulsion, mass, and dynamic models were implemented. The proposed solid propellant SLV design models are optimized to conduct an specific mission and represent an initiative that allows peru to rapid access into space.
- Abstract document
- Manuscript document
(absent)