Pegasus user’s guide – Orbital Pegasus User Manual
Page 79
Release 7.0
Apr 2010
A-1
Pegasus User’s Guide
APPENDIX A
PAYLOAD QUESTIONNAIRE
A Payload Questionnaire (PQ) is required from the payload organization for use in preliminary mission
analysis. The PQ is the initial documentation of the mission cycle and is needed 22 months before the
desired launch date. It is not necessary to fill out this PQ in its entirety to begin mission analysis. Simply
provide any available information and submit the document electronically via e-mail or fax.
See also other documents in the category Orbital Equipment:
- GMD Boost Vehicle (2 pages)
- GQM-163A Coyote (2 pages)
- Minotaur I (99 pages)
- Minotaur I (2 pages)
- Minotaur VI (2 pages)
- Minotaur IV (121 pages)
- Minotaur V (2 pages)
- Minotaur IV (2 pages)
- Minotaur-C (2 pages)
- Pegasus (2 pages)
- Antares (2 pages)
- Antares (99 pages)
- GEOStar-2 Bus (4 pages)
- GEOStar-3 Bus (2 pages)
- GEOStar Hosted Payloads (2 pages)
- SMF – Virginia (2 pages)
- SMF – Arizona (2 pages)
- LEOStar-3 Bus (4 pages)
- LEOStar-2 Bus (4 pages)
- Iridium NEXT (2 pages)
- Hingelock TEE Deployer Model 358 (2 pages)
- Hingelock TEE Deployer Model 5E9 (2 pages)
- Hingelock TEE Deployer Model 621 (2 pages)
- Hingelock TEE Deployer Model 625 (2 pages)
- Hingelock TEE Deployer Model 9843 (2 pages)
- Hingelock TEE Deployer Model T126 (2 pages)
- Overlap Dual-TEE Model 225 (2 pages)
- Overlap TEE Self-Deployer Model 1/2 OL-SD (2 pages)
- Overlap TEE Deployer Model 214 (2 pages)
- Wire Antenna Deployment Assembly Model 499 (2 pages)
- Wire Antenna Deployment Assembly Model 9842 (2 pages)
- Deep Space 1 (2 pages)
- Dawn (2 pages)
- RHESSI (2 pages)
- SORCE (2 pages)
- IBEX (2 pages)
- Coriolis (2 pages)
- FORMOSAT-3/COSMIC (2 pages)
- AIM (2 pages)
- Glory (2 pages)
- Landsat 8 (2 pages)
- OCO-2 (2 pages)
- ICESat-2 (2 pages)
- ICON (2 pages)