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Delta capability for launch of communications satellitesThe evolution of capabilities and the current performance levels of the Delta launch vehicle are outlined. The first payload was the Echo I passive communications satellite, weighing 179 lb, and placed in GEO in 1960. Emphasis since then has been to use off-the-shelf hardware where feasible. The latest version in the 3924 first stage, 3920 second stage, and Pam D apogee kick motor third stage. The Delta is presently equipped to place 2800 lb in GEO, as was proven with the 2717 lb Anik-D1 satellite. The GEO payload placement performance matches the Shuttle's, and work is therefore under way to enhance the Delta performance to handle more massive payloads. Installation of the Castor-IV solid motor separation system, thereby saving mass by utilizing compressed nitrogen, rather than mechanical thrusters to remove the strap-on boosters, is indicated, together with use of a higher performance propellant and a wider nose fairing.
Document ID
19840032857
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Grimes, D. W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Russell, W. A., Jr.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Kraft, J. D.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1982
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
84A15644
Distribution Limits
Public
Copyright
Other

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