elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Critical Analysis of Rocket Lab Neutron Launcher and Missions

Callsen, Steffen (2022) Critical Analysis of Rocket Lab Neutron Launcher and Missions. Project Report. SART TN-004/2022. 47 S.

Full text not available from this repository.

Abstract

Neutron is a two-stage launcher currently in development by the US-New Zealand company Rocket Lab. It is an innovative design featuring unique characteristics like a fixed fairing, an enclosed hung upper stage, fully carbon fiber structure and reusability via return-to-launch-site without an atmospheric entry burn. In order to analyze the impact of these features, this study is a critical analysis of the Neutron launcher based on the data available as well as numerous in-house calculations and assessments.

Item URL in elib:https://elib.dlr.de/185517/
Document Type:Monograph (Project Report)
Additional Information:Das PDF ist auf Anfrage bei RY-SRT erhältlich!
Title:Critical Analysis of Rocket Lab Neutron Launcher and Missions
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Callsen, SteffenUNSPECIFIEDhttps://orcid.org/0000-0002-5481-5403UNSPECIFIED
Date:4 March 2022
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:47
Status:Published
Keywords:Rocket Lab, Neutron, RTLS, CFRP, LOX/LCH4
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Systems Analysis Space Transport (SART)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Callsen, Steffen
Deposited On:07 Mar 2022 08:50
Last Modified:07 Mar 2022 08:50

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.