session 7

Title

Small Launchers: Concepts and Operations

Description

Discussion of existing, planned and future Launchers for small payloads ranging from 1500 kg to as low as 1 kg into Low Earth Orbit. Includes innovative solutions such as airborne systems, evolutions from sub-orbital concepts, combinations of existing / emerging elements and new elements, reusable, partially reusable and expendable concepts, and flexible, highly responsive concepts. Includes mission operations, design, development, and specific constraints

Date

2014-10-02

Time

14:45

Room

701B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Virgin Galactic's Dedicated Launch Vehicle for Small Satellites

accepted

20'

confirmed

Mr. William Pomerantz

Virgin Galactic L.L.C

United States

2

Small satellites missions by SOAR suborbital vehicle

accepted

20'

confirmed

Mr. Laurent Gathier

Dassault Aviation

France

3

Torogoz Sounding Rocket for El Salvador

accepted

20'

confirmed

Mr. Luis Salaverria

El Salvador

4

Super Strypi – Responsive Small Launch

accepted

20'

withdrawn

Mr. Mark Kaufman

Aerojet Rocketdyne

United States

5

light launch vehicle for operative launches of spacecrafts into the earth orbit

accepted

20'

confirmed

Dr. Volodymyr Kukushkin

State Enterprise "PA Southern Machine-Building Plant named after A. M. Makarov"

Ukraine

6

The Further Evolution Plan of Japan’s Epsilon Launch Vehicle

accepted

20'

confirmed

Prof. Yasuhiro Morita

Japan Aerospace Exploration Agency (JAXA), ISAS

Japan

7

Spartan - Nano-Launch Vehicle Concept

accepted

20'

withdrawn

Mr. Mark Kaufman

Aerojet Rocketdyne

United States

8

solid propellant space launch vehicle development program for peru – a proposal

accepted

20'

withdrawn

Dr. Fredy Villanueva

Conida - Space Agency of Peru

Peru

9

Styx: a student's project on airborne rocket systems

accepted

20'

confirmed

Mr. Bertrand Bocquet

ESTACA

France

10

Lean and Reliable Small Launcher - Design of Solid Rocket Booster and LOX/LNG Based Air Launched System

accepted

20'

withdrawn

Mr. Ali Butt

University of Alabama in Huntsville

United States

11

Small Low-cost Launch Vehicle Concept Design Based on Existing Solid Rocket Motors

accepted

20'

withdrawn

Dr. Dajun Xu

Beihang University

China

12

Balloon Launch - A Solution for Cheap Launch of Micro/Nano/Pico-Satellites

accepted

confirmed

Mr. Seyed Ali Nasseri

Space Generation Advisory Council (SGAC)

Canada