A new paradigm for the development and use of small platforms in future space missions is proposed, compared to the traditional approach, based on low cost development, commercial-off-the-shelf technology and launch as an auxiliary payload. The new scenario for the development and use of small satellites is based on three elements: first, a focus on the possible missions, and related requirements, suited for small spacecraft, including constellation and formation missions or missions integrated with larger space assets; second, the possibility of air launch, for independent access to space, responsiveness, and confidence of launch operations; third, a high tech approach both for the bus and its payload, including assembly, integration and testing technologies - including plug and play avionics – also for the purpose of in-flight demonstration and testing of new space technology suitable for larger spacecraft.
High tech small sat missions with air aunch capabilities / Gaudenzi, Paolo. - In: AEROTECNICA MISSILI E SPAZIO. - ISSN 0365-7442. - 90 (2-3):(2011).
High tech small sat missions with air aunch capabilities
GAUDENZI, Paolo
2011
Abstract
A new paradigm for the development and use of small platforms in future space missions is proposed, compared to the traditional approach, based on low cost development, commercial-off-the-shelf technology and launch as an auxiliary payload. The new scenario for the development and use of small satellites is based on three elements: first, a focus on the possible missions, and related requirements, suited for small spacecraft, including constellation and formation missions or missions integrated with larger space assets; second, the possibility of air launch, for independent access to space, responsiveness, and confidence of launch operations; third, a high tech approach both for the bus and its payload, including assembly, integration and testing technologies - including plug and play avionics – also for the purpose of in-flight demonstration and testing of new space technology suitable for larger spacecraft.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.