DocumentCode
324473
Title
Intrepid-a low cost small satellite launcher
Author
French, James R. ; Ingersoll, Thomas
Author_Institution
Rocket Dev. Co., Los Alamitos, CA, USA
Volume
3
fYear
1998
fDate
21-28 Mar 1998
Firstpage
167
Abstract
Small low-cost satellites still lack reliable, inexpensive access to space which can be available on short notice. Piggybacking with large satellites means scheduling, priority, and orbit access problems. The currently available launchers do not offer acceptable prices. Universal Space Lines (USL) and Rocket Development Company (RDC), recognizing this problem, began conceptual design of a low cost launch vehicle in late 1996. RDC is now in the early stages of development of this small, low-cost expendable launch vehicle called “Intrepid“. USL will be the operator, offering space transportation services to the industry. The two-stage Intrepid, using the liquid oxygen/liquid hydrogen propellant combination, is targeted for payloads up to about 1,100 lb for eastward launches in its basic form. Higher capability derivative vehicles with payload capability over 6000 lb, are also being designed. Construction is primarily composite in the interest of high production and low unit cost. Maximum use is made of existing electronic components in order to minimize development
Keywords
aerospace propulsion; artificial satellites; 1100 lb; 6000 lb; Intrepid; Piggybacking; Rocket Development Company; composite; cost; electronic components; flight performance; liquid oxygen/liquid hydrogen propellant; low cost launch vehicle; low unit cost; orbit access; payloads; priority; satellite launcher; scheduling; two-stage Intrepid; Aerospace industry; Construction industry; Costs; Hydrogen; Job shop scheduling; Payloads; Rockets; Satellites; Space vehicles; Transportation;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 1998 IEEE
Conference_Location
Snowmass at Aspen, CO
ISSN
1095-323X
Print_ISBN
0-7803-4311-5
Type
conf
DOI
10.1109/AERO.1998.685793
Filename
685793
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